KR20150144237A - Apparatus for detecting movement of an object - Google Patents

Abstract

The apparatus for detecting movement of an object according to the present invention includes: a transmitter and a transmitting antenna radiating an electromagnetic signal of one frequency band among X-band, K-Band, or Ka-band; a receiving antenna or a receiver receiving the reflected electromagnetic signal which is performed Doppler frequency bias from a moving object; a signal processor calculating a moving parameter of the moving object from the signal inputted from the receiver; and a control unit controlling the signal inputted from the signal processor to display.

Description

[0001] APPARATUS FOR DETECTING MOVEMENT OF AN OBJECT [0002]

The present invention relates to an apparatus for detecting movement of an object.

A device for detecting the movement of an object has been applied in various fields. Typically, in the case of screen golf, when a user hits a golf ball indoors, the speed and the trajectory of the golf ball are sensed and displayed on a screen to provide a realistic image as if playing golf on a real golf course.

However, such an apparatus for detecting the movement of an object has a problem that it can not be applied to a predetermined object other than a predetermined object by forming a tape or paint on a golf ball and analyzing it by detecting it with a radar.

In addition, when using the image acquisition method, not only the accuracy is degraded but also there is a limit to detecting the movement trajectory of the moving object in the outdoor.

The present invention provides an apparatus for detecting movement of an object that can accurately measure movement parameters of an object moving in the room as well as indoors.

The present invention provides an apparatus for detecting movement of an object with reduced power consumption.

The present invention provides an apparatus for detecting movement of an object with improved accuracy.

The apparatus for detecting movement of an object according to the present invention includes: a transmitter and a transmitter for radiating an electromagnetic signal in a frequency band of X-band, K-band, or Ka-band to a moving object; A receiving antenna and a receiver for receiving an electromagnetic signal reflected by the moving object and having a Doppler frequency shift; A signal processor for calculating a moving parameter of the moving object from a signal input from the receiver; And a controller for controlling the signal input from the signal processor to be displayed.

The present invention can provide an apparatus for detecting movement of an object that can accurately measure movement parameters of an object moving not only indoors but also outdoors.

The present invention can provide an apparatus for detecting movement of an object with reduced power consumption.

The present invention can provide an apparatus for detecting movement of an object with improved accuracy.

1 and 2 are views showing an apparatus for detecting movement of an object according to an embodiment of the present invention.
FIG. 3 is a diagram illustrating an example in which an object movement sensing apparatus according to an embodiment of the present invention is used in golf, and FIG. 4 is an example in which an object movement sensing apparatus according to an embodiment of the present invention is used in baseball Fig.
FIG. 5 is a diagram illustrating an arrangement of a phase comparison monopulse antenna in an apparatus for detecting movement of an object according to an embodiment of the present invention.
6 is a view for explaining an operation of a phase comparison monopulse antenna in an apparatus for detecting movement of an object according to an embodiment of the present invention.
FIG. 7 is a diagram for explaining the measurement of the gaze speed of a moving object using the apparatus for detecting movement of an object according to the embodiment of the present invention.
8 is a view for explaining the measurement of a velocity point of a moving object flying using an object movement detecting apparatus according to an embodiment of the present invention.
FIG. 9 is a diagram illustrating measurement of an azimuth angle, an altitude angle, and a launch angle of a moving object flying using an apparatus for detecting movement of an object according to an embodiment of the present invention.
10 is a view for explaining the measurement of the firing time and the initial firing rate of a moving object flying using an apparatus for detecting movement of an object according to an embodiment of the present invention.
FIG. 11 is a diagram for explaining the measurement of the rotation speed of an object flying while rotating in an object movement detecting apparatus according to an embodiment of the present invention.
12 is a view for explaining the measurement of the rotational speed of an object flying while performing a back spin and a side spin in a counterclockwise direction in an apparatus for detecting movement of an object according to an embodiment of the present invention.
FIG. 13 is a view for explaining the rotation speed of an object flying in a top-and-side spin in a clockwise direction in an apparatus for detecting movement of an object according to an embodiment of the present invention.
FIG. 14 is a diagram for explaining the measurement of the rotational speed of an object flying in a counterclockwise direction about a left rotation axis in an object movement detecting apparatus according to an embodiment of the present invention. FIG.
FIGS. 15 and 16 are diagrams for explaining measurement of a moving parameter of a moving object in an apparatus for detecting movement of an object according to an embodiment of the present invention.
FIG. 17 is a view for explaining an apparatus for detecting movement of an object according to another embodiment of the present invention, and FIG. 18 is a view for explaining a trigger signal generation of a 3-dimensional phased array Doppler radar in an apparatus for detecting movement of an object according to another embodiment of the present invention Fig.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS Hereinafter, an apparatus for detecting movement of an object according to an embodiment of the present invention will be described in detail with reference to the accompanying drawings.

In an embodiment of the present invention, an object can be any moving object. In particular, an embodiment of the present invention discloses an apparatus for detecting movement of an object in flight.

For example, an object may be a sport ball such as a golf ball, a baseball ball, a soccer ball, a basketball ball, a tennis ball, an arrow fired from a bowstep by an archer, a shot fired from a muzzle such as a rifle, Tools used to strike include clubheads, baseballs, tennis rackets, hockey sticks, and any objects that move or fly, such as athlete's hands and feet.

1 and 2 are views showing an apparatus for detecting movement of an object according to an embodiment of the present invention.

Referring to FIG. 1, an apparatus 100 for detecting movement of an object according to an embodiment of the present invention includes a transmission antenna 110, a sum reception antenna 120, an azimuth reception antenna 130, an altitude reception antenna 140, And includes a sound receiver 150, a transmitter 160, a sum receiver 170, an azimuth receiver 180, an altitude receiver 190, a trigger generator 200, a signal processor 210 and a controller 220.

The signal processor 210 includes an ADC 211, a DSP 212, a RAM 213, a memory 214, an external connector 215, a charging device 216 and a low voltage detector 217.

The control unit 220 includes a display unit 221, a controller 222, an application / analysis unit 223, and a user connector 224.

The ADC 211 receives the analog Doppler signal processed by the sum receiver 170, the azimuth angle receiver 180 and the altitude angle receiver 190 and the analog trigger signal generated by the trigger generator 200 as a digital signal And converts the input analog Doppler signal and the analog trigger signal into a digital Doppler signal and a digital trigger signal, respectively, at a predetermined sampling period, and transmits the digital Doppler signal and the digital trigger signal to the RAM 213.

The RAM 213 stores a digital Doppler signal and a digital trigger signal converted into a digital signal by the ADC 211.

The memory 214 stores a signal processing program for calculating a movement parameter for an object processed by the DSP 212 and data calculated in the signal processing program. The movement parameter may include at least one of a movement time, an initial movement speed, a movement angle, a movement speed, an acceleration, a movement distance, an altitude angle, an azimuth angle, a locus, a rotation speed, a rotation axis and a landing point of a moving object.

The DSP 212 calculates movement parameters of the object by a program driven by a predetermined algorithm built in the memory 214 using the digital Doppler signal and the digital trigger signal stored in the RAM 213 214).

The charging device 216 is a device for charging a voltage and is a power supply device for use without connecting to a commercial power source for a predetermined time in a place where it is difficult to use a commercial power source. In the embodiment of the present invention, it is used as a device for supplying power.

The low voltage detector 217 continuously monitors whether the voltage value charged in the charging device 216 is less than or equal to a predetermined threshold value and outputs an alarm signal that can be recognized by the user, And notifies the user of the recharging.

The external connector 215 is a device for signal processing in the DSP 212 and transmitting the data stored in the memory 214 to the controller 220. UART, Bluetooth, Wi-Fi, etc. are applied for wired and wireless communication .

The controller 220 may control the application parameter analyzer 223 in which the controller 222 stores a predetermined application / analysis program, based on the movement parameters calculated by the signal processor 210 received through the external connector 215, And displays the analyzed result on the display unit 221 by various methods such as numbers, graphs, graphics, and the like.

2, the transmit antenna 110, the sum receive antenna 120, the azimuth receive antenna 130, the altitude receive antenna 140, the acoustic receiver 150, the transmitter 160, the sum receiver 170, An azimuthal receiver 180, an altitude angle receiver 190, a trigger generator 200, and an ADC 211 are shown in more detail.

2, the transmitter 160 includes a dielectric resonator (DRO) 161, a power amplifier (PA) 162, a coupler (COUP) 163, and an isolator (ISO) .

The dielectric resonator 161 generates an electromagnetic signal of any one of the X-band, the K-band, and the Ka-band, and the power amplifier 162 amplifies the electromagnetic signal generated by the dielectric resonator 161 And transmits the amplified signal to the coupler 163. The power amplifier 162 controls the emission of the electromagnetic signal output from the transmitter 160 and controls the emission of the trigger detected by the trigger generator 200, And controls the emission of an electromagnetic signal emitted from the transmitter 160 through the signal processor 210 according to a signal.

The apparatus for detecting movement of an object according to an embodiment of the present invention has a structure capable of reducing power consumed by the transmitter 160.

In the first method, the power amplifier 162 constitutes a radiation beam controller, and the driving power is supplied to the power amplifier 162 through the radiation beam controller. In the absence of a signal, a structure may be used in which the power amplifier 162 operates in a standby mode in which power amplification is not performed, thereby controlling the emission of the electromagnetic signal output from the transmitter 160.

In a second method, a microwave switch may be disposed at a position connected to an input terminal or an output terminal of the electromagnetic signal of the power amplifier 162. Specifically, although not shown in FIG. 2, the dielectric resonator And a circuit for controlling electromagnetic signals radiated through the transmitter 160 by arranging a microwave switch (not shown) between the power amplifier 162 and the coupler 163 between the power amplifier 162 and the coupler 163, Can be configured. That is, the microwave switch can operate the signal output from the power amplifier 162 in the standby mode when there is no trigger signal detected by the trigger generator 200.

The coupler 163 includes a transmission output signal transmitted from the power amplifier 162 to the isolator 164 and a reception signal from the sum receiver 170, the azimuth receiver 180, and the altitude receiver 190 And outputs three signals having the same frequency and the same power level for driving the three mixers (MIX) 173, 183, and 193, respectively.

The isolator 164 induces impedance matching between the power amplifier 162 and the transmission antenna 110 and blocks external noise introduced through the transmission antenna 110 from flowing into the power amplifier 162, And transmits the amplified signal from the amplifier 162 to the transmission antenna 110 in a stable manner.

The transmission antenna 110 radiates the microwave signal output from the transmitter 160 toward an object moving (flying).

The received signal reflected by the object with the Doppler frequency shifts is received by the sum receive antenna 120, the azimuth receive antenna 130 and the altitude receive antenna 140, which are three receive antennas, 170, an azimuthal receiver 180, and an altitude angle receiver 190, respectively.

The summing receiver 170, the azimuthal receiver 180 and the altitude angle receiver 190 may all be composed of the same electronic circuit and may be implemented as low noise amplifiers (LNAs) 171, 181 and 191, band pass filters (BPF) 172, 182, 192, mixers MIX 173, 183, 193, low pass filters (LPF) 174, 184, 194, automatic gain control amplifiers (AGC) 175, 185, 195, and the like.

The low-noise amplifiers 171, 181, and 191 amplify a received signal received from an antenna connected to one of the three receiving antennas, which is reflected by the Doppler frequency shift in an object moving (flying) The pass filters 172, 182 and 192 remove noise introduced from an antenna having a predetermined bandwidth and connected to one of the three receive antennas and pass only low noise amplified signals from the low noise amplifiers 171, 181 and 191, and the mixers 173, 183 and 193 Mixes one of the three output signals output from the coupler 163 constituting the transmitter 160 with the signal passed through the band pass filters 172, 182 and 192 to output an analog Doppler signal, The filters 174, 184, and 194 output high frequency components that can be included in the analog Doppler signals output from the mixers 173, 183, The automatic gain control amplifiers 175, 185, and 195 amplify the low-level analog Doppler signals output from the low-pass filters 174, 184, and 194 to a constant high-gain signal, To the ADC 211.

The sound generator 150 includes a sound wave amplifier 201 and a trigger signal discriminator 202. The trigger sound generator 200 includes a sound wave amplifier 201 and a trigger signal discriminator 202. [ And the trigger signal discriminator 202 detects a trigger signal of the signal outputted from the sonic amplifier 201. The trigger signal discriminator 202 amplifies the low- The amplitude is compared with a predetermined threshold value, and a trigger signal is generated when the amplitude of the signal exceeds a threshold value.

The object movement detecting apparatus according to an embodiment of the present invention may be disposed at a predetermined distance from the point (firing point) at which the object starts moving, to the left, right, or rear, and may be a Doppler frequency- Calculates the movement parameters of the launched object in real time, analyzes the calculated movement parameters, and displays the analyzed results to the user in various ways such as numbers, graphs, graphics, and the like.

FIG. 3 is a diagram illustrating an example in which an object movement sensing apparatus according to an embodiment of the present invention is used in golf, and FIG. 4 is an example in which an object movement sensing apparatus according to an embodiment of the present invention is used in baseball Fig. However, the application of the present invention is not limited to golf or baseball, and can be applied to all moving objects.

Referring to FIG. 3, an apparatus 100 for detecting movement of an object according to an embodiment of the present invention may be a three-dimensional phased array Doppler radar capable of measuring a trajectory of a moving object.

When the golfer 300 hits the golf ball 320 in the stopped state using the golf ball 310, the golf ball 321 moving (flying) has a trajectory 330 when flying in the three-dimensional space, The transmission signal 340 emitted from the movement sensing apparatus of the present invention is reflected by a Doppler frequency shifted signal in the moving golf ball 321 and is received by the reception signal 350.

3, the reference plane 360 is a reference plane on which an object movement sensing apparatus 100, a golfer 300, and a golf ball 320 in a stopped state are located, and a ground on which an object or an apparatus for emitting an object is disposed .

The object movement sensing apparatus 100 is disposed at a predetermined distance to the left, right, or rear of the initial position of the golf ball 320 in a stationary state on the reference plane 360 so as to be oriented And the golf ball 321 flying by the blow of the golfer 300 flies along the trajectory 330. The sound receiver 150 receives the golf ball 300 from the golf ball 310, 320).

And generates a trigger signal and provides the trigger signal to the signal processor 210. In the signal processor 210, a predetermined algorithm Controls the electromagnetic signal radiated from the transmitter 160 to radiate the transmitted signal 340 having a transmission frequency of f ₀ to the golf ball 321 flying through the transmission antenna 110, The received signal 350 reflected by the Doppler frequency shift in the Doppler frequency domain 321 is received by the sum receive antenna 120, the azimuth receive antenna 130 and the altitude receive antenna 140, The analog Doppler signals are transmitted to the sum signal receiver 210, the azimuth receiver 180, and the altitude angle receiver 190. The analog Doppler signals are transmitted to the signal processor 210, Golf balls (321) And transmits the calculated flight parameters to the control unit 220 to display the calculated flight parameters in a number or graph that can be recognized by the user.

4, the movement sensing apparatus 100 of the object is positioned at a predetermined distance to the left, right or rear of the batter 400 so as to be directed toward the expected flight path 430 of the baseball ball When the batter 400 hits the baseball bat 410 using the baseball bat 410, the sound receiving unit 150 of the movement sensing apparatus of the present invention senses the batter sound, A transmission signal radiated from an object movement sensing apparatus is reflected by a Doppler frequency shifted signal in a flying baseball 420 and is received, and the reflected and received signals are received by a sum reception antenna 120, an azimuth reception antenna 130 The received signals from the three receive antennas are transmitted to a summation receiver 170, an azimuth receiver 180 and an altitude angle receiver 190, and the three receivers Analog Doppler processed A logarithmic Doppler signal is transmitted to the signal processor 210 to calculate a flight parameter of the flying baseball 420 and the calculated flight parameters are transmitted to the control unit 220 so that a number or a graph .

The Doppler frequency-shifted signal is generated due to a phase change between the radar and a moving object. Such a phenomenon is referred to as a Doppler effect. The object movement sensing apparatus 100 radiates a radio wave having a transmission frequency f ₀ toward a moving object and receives a reflected reception signal by shifting the Doppler frequency in the moving object to generate a transmission signal 340 and a reception signal 350, The change of the phase in both directions is expressed by Equation (1).

(T) is the amplitude of the signal when the reflected signal is shifted to the Doppler frequency and the reflected signal is received by the movement sensing apparatus 100, f ₀ is the transmission frequency, and φ (t) 100) and the moving object, and the unit is radian.

At this time, when the distance between the movement sensing apparatus 100 and the moving object changes due to the movement of the moving object, that is, when the moving object moves toward or away from the movement sensing apparatus 100 , The phase φ (t) can be expressed by the following equation (2) due to the change in the distance R between the movement sensing apparatus 100 and the moving object.

The number of wavelengths included in the changed phase in both directions between the movement sensing apparatus 100 and the moving object can be expressed by the following equation (3): " (3) " ].

In Equation (3), ω _d = 2πf _d , and the change in the distance R with time means a speed, which can be expressed by Equation (4).

In Equation (4), V _r is a relative velocity occurring due to a change in the distance R between the movement sensing apparatus 100 and the moving object, is called a radial velocity, and the visual velocity V _r of the moving object is expressed by [ As shown in Equation (5), the gaze velocity V _r of the moving object can be obtained from the Doppler frequency f _d in proportion to the Doppler frequency f _d observed in the movement sensing apparatus 100.

In general, the movement sensing apparatus 100 and the moving object always move in a state of being displaced by an arbitrary viewing angle? _R without moving at a line of sight of 90 degrees, ), The error rate of cos (θ _r ) occurs with respect to the actual velocity V _act as shown in Equation (6), so that the signal processor compensates for the error by the cos (θ _r ).

FIG. 5 is a diagram illustrating an arrangement of a phase comparison monopulse antenna in an apparatus for detecting movement of an object according to an embodiment of the present invention.

5, the antenna of the moving object movement sensing apparatus 100 includes a transmission antenna 110 for transmitting a transmission signal with a predetermined radiation beam width to a moving object moving or flying in a three-dimensional space, Receiving antenna 120, an azimuth-receiving antenna 130, and an altitude-angle receiving antenna 140, which are designed to have the same electrical standard for detecting azimuth and elevation angles by receiving a received signal reflected by a Doppler frequency shift in a moving object, Phase comparison is arranged according to the monopulse principle.

In order to measure the azimuth angle of the moving object flying in the radiation beam, the sum receive antenna 120 and the azimuth receive antenna 130 are spaced apart from each other by an interval d _AZ , and an altitude angle of the moving object The sum receive antenna 120 and the altitude receive antenna 140 are spaced apart from each other by an interval d _EL .

6 is a view for explaining an operation of a phase comparison monopulse antenna in an apparatus for detecting movement of an object according to an embodiment of the present invention.

The two reception antennas 610 and 620 arranged in the phase comparison monopulse principle are spaced apart by a distance d. The two reception antennas are connected to the sum reception antenna 120, the azimuth reception antenna 130, And may correspond to the receiving antenna 120 and the altitude receiving antenna 140. [

6, in the radiation beam, the two signals 630 and 640 reflected and received by the Doppler frequency shift in the moving object 600 flying at a long distance are parallel, and are received by the receiving antennas 610 and 620 at angles? _P The signals 630 and 640 from the two receiving antennas 610 and 620 are received with a path length difference? R = dsin (? _P ). When the signals 630 and 640 are expressed by an electrical wavelength relationship, The phase difference between the two received signals becomes equal to Equation (7).

Therefore, the phase difference between the two signals that are shifted in the Doppler frequency shift and received by the two receive antennas 610 and 620 are shown in Equation (8).

In the above equations (7) and (8),? ₀ is the wavelength of the transmission frequency f ₀ , and using the antennas arranged according to the phase comparison monopulse principle, The azimuth and elevation angle of the moving object can be measured and the trajectory of the moving object can be measured using the measured azimuth angle and elevation angle.

The antenna disposed in accordance with the phase comparison monopulse principle in the apparatus 100 for detecting movement of an object according to an embodiment of the present invention may have the same size in any one of X-band, K-band, or Ka- The antenna having the directivity characteristic is not limited to a microstrip patch antenna. An antenna structure well known to those skilled in the art, such as a horn antenna, a parabolic antenna, and a slot antenna, However, since the microstrip patch antenna can be fabricated on a dielectric substrate such as a printed circuit board or a Teflon substrate, it is advantageous to make the movement detecting apparatus 100 lightweight and slim.

The microstrip patch antenna may be formed by using a thin metal plate such as copper on a dielectric substrate having a predetermined thickness or by plating gold or silver having excellent electrical conductivity. A microstrip patch antenna fabricated by forming a predetermined pattern on a substrate or the like is used to protect the microstrip patch antenna from oxidation and corrosion due to impact from outside and contact with rain, snow, dust and other chemicals, A radome may be formed to emphasize the aesthetic effect of the sensing device 100. The radome may use the same substrate as the dielectric substrate used for fabricating the microstrip patch antenna or may be formed of a material such as FR-4 (Flame Retardant composition 4) The use of a heterogeneous dielectric substrate or a vision that does not include metallic powders It may be formed using a conductive paint, using paint that does not contain carbon particles, or using a dielectric material that does not electrically affect the radiation properties of the antenna.

FIG. 7 is a diagram for explaining the measurement of the gaze speed of a moving object using the apparatus for detecting movement of an object according to the embodiment of the present invention.

7, the receiving antenna of the object movement sensing apparatus 100 is located at the origin of the three-dimensional coordinates of the X, Y, and Z axes, and moves the moving locus 702, 704 within the observation range of the receiving antenna at the actual velocity When the received signals reflected by the moving objects 701 and 703 flying at V _act are reflected by the Doppler frequency and are received by the altitude angle _EL and the azimuth angle beta _AZ , The gaze speed V _r of each of the display units 701 and 703 is expressed by Equation (9).

As can be seen from Equation (9), the line-of-sight velocity V _r observed from the reception antenna is different from the actual velocity V _act, and an error occurs by the cosine function of the azimuth angle? _AZ and the altitude angle? _EL , The actual velocity _Vact of the moving object flying at V can be calculated by dividing the visual velocity V _r by the cosine function error.

8 is a view for explaining the measurement of a velocity point of a moving object flying using an object movement detecting apparatus according to an embodiment of the present invention.

8, a moving object follows the trajectory 801 in the radiation beam θ _BEL (800) of the object movement sensing apparatus 100, and an electromagnetic signal having a transmission frequency f ₀ toward the moving object When the beam is radiated, the receiver receives the reflected signal at the receiver and acquires the data at a predetermined sampling time interval in the signal processor. The obtained data is converted into a radiation beam &thetas; _BEL can be expressed in a number of speed points (velocity point) (802) having a predetermined sampling time interval, the time difference between the plurality of speed points, any two speed points Δt = t _n-2 -t _{n -1} is constant with sampling time.

FIG. 9 is a diagram illustrating measurement of an azimuth angle, an altitude angle, and a launch angle of a moving object flying using an apparatus for detecting movement of an object according to an embodiment of the present invention.

As shown in FIG. 9, the altitudinal velocity V _EL at an arbitrary velocity point of the moving object flying along the trajectory 801 in the altitude angular radiation beam θ _BEL (800) is given by Equation (10) The square root of the horizontal velocity component V _ELH plus the square of the vertical velocity component V _ELV can be obtained.

If the altitude firing angle of the moving object flying at an arbitrary velocity point in the altitude each radiation beam [theta] _BEL (800) is [theta] _LEL , the horizontal velocity component V _ELH and the vertical velocity component V _ELV at the velocity point, Can be expressed as Equation (11).

High elevation balsagak of the moving object flying at any speed point within each radiation beam θ _BEL (800) is also θ _LEL is [Equation 11] and [equation 12], the horizontal velocity of the high velocity V _EL component of V _ELH and the vertical direction velocity component V _ELV , it can be obtained by an arc tangent function as shown in Equation (13).

Through this procedure, at the arbitrary velocity point in the azimuth radiation beam width θ _{BAZ (} not shown), the azimuthal direction launch angle θ _LAZ of the moving object is expressed by the horizontal direction component V _AZH and the vertical direction component V _AZV of the azimuth directional speed V _AZ And can be obtained by an arc tangent function as shown in [Equation 14].

Therefore, when both [Equation 13] and [Equation 14] are used, the emission angle and the trajectory in the azimuth direction and the elevation angle direction can be continuously obtained.

10 is a view for explaining the measurement of the firing time and the initial firing rate of a moving object flying using an apparatus for detecting movement of an object according to an embodiment of the present invention.

As shown in FIG. 10, the initial firing velocity V ₀ and the firing time t ₀ of the flying object at the flying time are set to a minimum of at least three velocity points measured in the radiation beam of the object movement sensing apparatus 100, When a time point at which the robot meets the axis extends to the firing point t ₀ by using a quadratic curve fitting or regression analysis or an algorithm known to those skilled in the art, a launching device for firing a moving object obtains a firing time t ₀ at which the moving object is struck And the initial firing velocity V ₀ of the moving object at the time of the firing time t ₀ can also be obtained.

FIG. 11 is a diagram for explaining the measurement of the rotation speed of an object flying while rotating in an object movement detecting apparatus according to an embodiment of the present invention.

As shown in FIG. 11, an electromagnetic beam having a transmission frequency of f ₀ is radiated to a spherical moving object flying in the radiation beam while rotating at a predetermined distance R ₀ A spherical moving object with respect to the movement sensing apparatus 100 is positioned at an altitude angle? _EL = 0 ° and an azimuth angle? _AZ = 0 °, that is, at a position where both the movement sensing apparatus 100 and the spherical moving object are two- The change in the linear distance from the moving object to the moving object 100 that emits a continuous wave is reflected from the moving object and is detected by the signal received from the moving object sensing apparatus 100 .

When a spherical moving object having a radius r _b and a center C _b rotates at a rotational speed ω _s while flying at a visual velocity V _r , the distance R from the motion sensor 100 to an arbitrary point P _A on the spherical moving object Is a time-varying function expressed by Equation (15).

In the above equation (15), R ₀ is the distance from the movement sensing apparatus 100 to the center C _b of the spherical moving object having the radius r _b , and θ _s0 is the initial rotation angle. Using Equation (15), the wave radiated from the motion sensing device 100 is reflected by the spherical moving object and expressed in the received phase as shown in Equation (16).

Therefore, the signal reflected from the moving object and received by the movement sensing apparatus 100 is expressed by Equation (17).

When Equation 17] Φ (t) in the expression in terms of the time-varying phase ((時變位相)), the rotational frequency ω _s of this, the moving object can be written as [Equation 18].

[Equation 18] is written in the form of Fourier series expansion, as in Equation 19,

In Equation (19), n is an integer, and c _n is a Fourier coefficient, as shown in Equation (20).

Equation (20) is an n-th order Bessel function of the first kind, and Equation (21) is obtained by substituting Equation (20) into Equation (19).

(21) is a frequency modulation signal represented by a harmonic line spectrum in which a rotational frequency f _s = ω _s / 2 π is paired around a frequency f ₀ , and FM The instantaneous frequency of the signal is obtained by differentiating the phase? (T) of [Expression 16] with respect to time as expressed by Equation (22).

In Equation 22] f _d is the Doppler frequency is derived from the projectile flying in the radial velocity V _r, a change in frequency due to the rotation speed of the right ω _s, the maximum frequency shift _{(4π / λ 0) r b} ω _s .

The above will be described in more detail as follows.

12 is a view for explaining the measurement of the rotational speed of an object flying while performing a back spin and a side spin in a counterclockwise direction in an apparatus for detecting movement of an object according to an embodiment of the present invention.

As shown in Fig. 12, a spherical moving object having a radius r _b and a center C _b , which rotates at a rotation speed ω _s while flying at a visual velocity V _r in a straight line direction parallel to the movement sensing apparatus 100 As shown in Fig. 12 (a), back-spin in the anticlockwise direction or fly in the counter-clockwise direction as shown in Fig. 12 (b) When the movement sensing apparatus 100 emits a radar beam to the spherical moving object of FIGS. 12A and 12B, a plurality of (for example, two or more) spherical moving objects The signal received by the motion sensing apparatus 100 due to the Doppler frequency shift at any one of the points P ₁ , P ₂ , P ₃ , P ₄ and P ₅ can be expressed by the following equation (23) , [Equation 24], [Equation 25], [Equation 26] and [Equation 27].

12 (a) and 12 (b), a point P ₃ on a spherical moving object flying at 0 ° with respect to the beam radiated from the movement sensing apparatus 100, There is only a Doppler frequency f _d due to the visual velocity V _r of the moving object.

At an arbitrary point between the points P ₁ and P ₃ and at any point between the points P ₃ and P ₅ , the rotational speed? _S of the spherical moving object and the visual velocity V _r are present together, 12 (a) and 12 (b) form a horizontal axis and a vertical axis, respectively, with respect to the beam radiated from the point P ₁ to the point P ₃ , And a point P _{2 which} is located at a point between the point P ₃ and the point P ₅ on the basis of the rotation axis exists in a backspin or a side spin and a backspin or a side spin In point P ₄ , there exists a frequency component as shown in [Equation 26], and the spherical movement At the rotating point P ₁ and the point P _{5 on} the object corresponds to a point where the visual velocity V _r of the spherical moving object and the rotational speed ω _s component rotating at right angles to the rotational axis exist, Focusing on any one of the axis because the rotation in the counterclockwise direction, so that in the P ₁ rotation speed ω _s direction is opposite to the radial velocity V _r direction is expressed as [equation 23], the rotation speed at the point P ₅ ω _s Direction is the same as the gaze speed V _r direction, and therefore, it is expressed as: " (27) "

12 (c) is a line spectrum of the Doppler frequency obtained by using the above-mentioned [Expression 23] to [Expression 27] in the frequency domain and is generated in a spherical moving object flying while rotating in a counterclockwise direction The spectrum has a Doppler frequency f _d corresponding to the visual velocity V _r and the rotation frequency f _sp5 is the highest at the point P ₅ since the rotation frequency f _sp1 at the point P ₁ is the lowest and the rotation frequency at the point P ₃ is zero .

FIG. 13 is a view for explaining the rotation speed of an object flying in a top-and-side spin in a clockwise direction in an apparatus for detecting movement of an object according to an embodiment of the present invention.

As shown in Fig. 13, top spin in the clockwise direction as shown in Fig. 13 (a) in a straight line direction parallel to the movement sensing apparatus 100, When a radar beam is radiated to a spherical moving object flying while side-spinning in the clockwise direction, a description is made in the same manner as in the spherical moving object flying backward in the counterclockwise direction or side-spin in the counterclockwise direction However, in the case of Equations (23) and (24), and in the case of Equations (26) and (27), the + sign and the - symbol are changed to each other, Only the difference that the order is changed as shown in (c) of FIG. 13 becomes the same as the above description.

FIG. 14 is a diagram for explaining the measurement of the rotational speed of an object flying in a counterclockwise direction about a left rotation axis in an object movement detecting apparatus according to an embodiment of the present invention. FIG.

The rotation axis of the spherical moving object which is backspin in the counterclockwise direction in the direction of the straight line parallel to the movement detection device 100 or side spin in the counterclockwise direction is shown in FIG. 14 (a) , The same principle is the same as the cosine function corresponding to the tilt angle of the rotation axis in the equations (21a) to (21e) When the rotation axis of a spherical moving object which is backspin or side spin in the counterclockwise (counterclockwise) direction is rotated by an arbitrary angle to the right, there is a difference in the cosine function corresponding to the tilt angle of the rotation axis. And the principle of whether the inclination of the rotation axis of the two cases is the right side or the left side is changed in principle.

Further, when the rotation axis of the spherical moving object which is top-spun or side-spun in the clockwise direction in the direction parallel to the movement sensing apparatus 100 is rotated by being tilted to the left or right by an arbitrary angle, 23] to [Equation 27] by the cosine value corresponding to the tilt angle of the rotation axis, but the same principle can be similarly explained.

In order to measure the rotational speed of a rotating flying object in the object movement detecting apparatus 100 according to the embodiment of the present invention, it is possible to perform the following procedure.

First, a window function having a predetermined width is applied to a Doppler signal sampled at a predetermined sampling period in the signal processor 210 of the object movement sensing apparatus 100 and converted into a digital signal, and N signals (FFT) for each of the fast Fourier transformed signals, obtains an energy spectrum for each of the fast Fourier transformed signals, synthesizes them in a two-dimensional plane of time-frequency, Extract the line spectrum.

The FM signal spectrum is a Doppler signal generated from a rotating moving object. The Doppler frequency f _D is a Doppler frequency that is generally shifted by a visual velocity V _r (moving motion) symmetrical to the rotation frequency f _s of a 2M etc. _spM f, the line spectrum of the interval (等間隔) ... _{, f sp2, f sp1, f} d, f sp1 ', f sp2', ... , and f _spM '(where M = 1, 2, 3, ...), and when grasping the frequency components of each of the 2M line spectra, or knowing the modulation bandwidth and the like, Can be known.

In the first method, the Doppler spectrum frequency f _d is obtained from the energy spectrum signal obtained from the two-dimensional plane of the time-frequency, and the Doppler frequency f _d is used as the center frequency, and the FM frequency line spectrum FM bandwidth obtain the BW _FM, finding the FM bandwidth BW plurality of line spectrum center frequency of the Doppler frequency f _d any of a number of peak (peak) value of the energy ray spectra in the left and Yiwu symmetry, including from within the _FM, And the signal having the highest peak value obtained is a Doppler line spectrum frequency f _d due to the visual velocity V _r of the spherical moving object, Each signal arranged at regular intervals, regardless of whether it is the line spectrum of the sideband signal, The divided by the amplitude of the energy ray-spectrum signal having a high peak value, normalized, and the line doppler a normalized each value spectrum frequency f _d center to left and right order normalization arranged in the interval, an array, each such as the And the obtained FM bandwidth BW _FM is compared with the n-th order one-kind Bessel function table stored in the form of a reference table, and is calculated by applying [Expression 28] according to Carson's rule.

In the above equation (28), f _S is a frequency modulation signal, i.e., a rotation frequency, and β _FM is a frequency modulation index (FM Index), which is a factor of the _n- th order Bessel function J _n (β _FM ).

A second method, the time from the energy spectrum signal obtained from a two-dimensional plane of the frequency, to obtain a Doppler frequency frequencies f _d and the line spectral energy caused by translation of the projection surface (a moving object), around the f _d The difference frequency of the two frequencies obtained by _finding the frequencies of the _{symmetrically arranged} M-th line spectra f _spM and f _spM 'and the energy of the corresponding line spectrum, and obtaining the difference frequency Δf _spM = | f _spM -f _spM ' | , The number of line spectra existing in the symmetric section is 2M, and the difference frequency? _{F spM} is divided by the line spectrum number 2M.

As a third method, a line spectrum is obtained by auto-correlating the time series data converted into the digital signal, and the obtained line spectrum is subjected to wavelet decomposition in the same manner as the above methods The frequency or the rotational speed of the moving object flying in the course of the rotation in the line spectrum of the Fourier-transformed FM signal can be obtained by averaging the values obtained by dividing the difference frequency, It can be obtained, using the method described above, based on the Doppler frequency f _d left, in any peak value, and detecting a harmonic of the rotation frequency of the right, the peak value or the rotation frequency of the detected Doppler frequency f _d And the normalized value is compared with the n-th order one-kind Bessel function table so that the stable and accurate rotation speed Alternatively, the rotation frequency can be obtained.

FIGS. 15 and 16 are diagrams for explaining measurement of a moving parameter of a moving object in an apparatus for detecting movement of an object according to an embodiment of the present invention.

15, when power is applied to the movement sensing apparatus 100, a check procedure set in the movement sensing apparatus 100 is performed (S110), and the transmitter 160, the receivers 170, 180 and 190, the DSP 212, The memory 214, the RAM 213, the control unit 220 and the like to check whether there is an abnormality, and if there is an abnormality, an alarm sound or an alarm sound that the user can recognize by using an output device such as a speaker or an LED And generates an optical signal, and operates in the measurement standby mode if the movement sensing apparatus 100 is normal (S120)

When the moving object is fired by the striking device in the radiation beam on the front face of the movement sensing apparatus 100, the sound sensing unit 150 of the movement sensing apparatus 100 senses a sound to be sounded A trigger signal is generated in the trigger generator 200 and transmitted to the signal processor 210 in operation S130. However, in another embodiment described later, the trigger signal may be generated by a trigger signal generated by the Doppler frequency Signals are simultaneously present in the trigger generator 200, and generates a trigger signal in the trigger generator 200 when both of the signals exist.

The signal processor 210 of the movement sensing apparatus 100 transmits a command signal to the transmitter 160 of the movement sensing apparatus 100 to emit a transmission signal and transmits the command signal to the transmitter 160 of the movement sensing apparatus 100, And radiates a transmission signal toward the moving object (S140)

The signal processor 210 samples the analog Doppler signals transmitted from the sum receiver 170, the azimuth receiver 180, and the altitude receiver 190, respectively, to collect digital Doppler signal data. The digital Doppler signal data is continuously collected in a receiver as a time-series signal (S150)

The movement sensing apparatus 100 calculates a movement parameter related to the moving object to be traveled and transmits the movement parameter to the control unit 220 of the movement sensing apparatus 100. The control unit 220 controls the application / 223), movement parameters of a moving object flying using the operation / analysis program of the baseball, a swinging action of a launching tool such as a club head or a baseball bat used in a firing process, and a moment of hitting a flying or moving object such as a baseball (S160) (S170). ≪ tb > < TABLE >

At the same time that the step 170 is completed, the movement sensing apparatus 100 recognizes the user to stop the measurement. If there is no response from the user within the predetermined time, the mobile sensing apparatus 100 waits for the next firing in the measurement standby mode.

FIG. 16 is a flow chart illustrating in detail the steps from the data acquisition step (step S150) to the object flight information analysis step (step S160) in the flowchart of FIG. 15, The digital Doppler signal data is sampled at each predetermined sampling period by sampling each of the analog Doppler frequency signals received from the three receivers in real time in order to generate a velocity spectrum of the analog Doppler signal generated from the moving object, And stores it in the RAM 213 (S210)

The time series signal is generated by dividing or superimposing the signals in a predetermined time interval using a predetermined window function (S220)

Into a frequency spectrum, which is a signal in the frequency domain, using Fast Fourier Transform (S230)

For each frequency-converted signal, two-dimensional data of the time-frequency dimension is obtained, and two-dimensional data of the obtained time-frequency dimension is calculated as two-dimensional velocity data of the time-velocity dimension. (S240)

The movement parameters of the flying moving object are calculated using the plurality of velocity points (S250)

In another embodiment of the present invention

FIG. 17 is a view for explaining an apparatus for detecting movement of an object according to another embodiment of the present invention, and FIG. 18 is a view for explaining a trigger signal generation of a 3-dimensional phased array Doppler radar in an apparatus for detecting movement of an object according to another embodiment of the present invention Fig.

In the embodiment described with reference to FIG. 1, the object movement sensing apparatus 100 senses a sound generated when a moving object launching apparatus hits a stationary or moving moving object in the acoustic receiver 150, The moving object sensing apparatus 100 may be configured to generate a trigger signal to measure a velocity from a moving object that the motion sensing apparatus 100 is flying, Is set to be greater than a predetermined threshold value set in the trigger generator 200 of the movement sensing apparatus 100 or a noise due to physical vibration in the reference plane is set in the trigger generator 200 The noise generated by the thunder or other natural phenomenon is greater than a predetermined threshold value set in the trigger generator 200, If the physical noise is greater than a predetermined threshold value set in the trigger generator 200, the movement sensing apparatus 100 can sense one of the noises, and if the sensed noise is detected in the predetermined It is possible that the movement sensing apparatus 100 may misjudge such a noise as a moving object being fired on the reference plane on which the movement sensing apparatus 100 is disposed, Lt; / RTI >

Accordingly, in another embodiment of the present invention, as shown in FIG. 17, the movement of the launch device such as a club head in the radiation beam of the movement sensing apparatus 1000 or the Doppler frequency A first trigger generator 201 for generating a first trigger signal Trg # 1 when both a signal and a sound signal detected by the sound receiver 150 are generated, and for the generated Doppler frequency signal, The speed calculated in the predetermined time period is a speed generated by a moving object such as a club head or a flying object such as a golf ball, If it is determined within the predetermined speed range that the speed calculated by the other arbitrary moving object or the flying object is within the predetermined speed range, A second trigger generator is configured to generate a second trigger signal Trg # 2, which is implemented in software in the signal processor 210, using both the first trigger signal and the second trigger signal And generates an actual trigger signal in the signal processor 210.

Accordingly, since the moment when the moving object is fired is recognized in the movement sensing apparatus 1000 according to another embodiment of the present invention, the trigger error can be minimized, and it is possible to recognize the time when the moving object is fired more stably, .

FIG. 18 is a flowchart illustrating a trigger signal generation process of an object movement detection apparatus 1000 according to another embodiment of the present invention. Referring to FIG. 18, It is determined whether both the Doppler signal generated by the moving object and the sound generated by the launch device and the moving object are generated (S310)

In step S320, a Trg # 1 signal, which is a first trigger signal, is generated and transmitted to the movement device or the launch device of the movement device 1000, The signal processor calculates a velocity for a predetermined time interval with respect to the Doppler frequency signal generated by the moving object struck by the moving object, and determines in step S330 whether the velocity obtained in the predetermined time interval is within the specified velocity (S340), the second trigger signal Trg # 2 is generated when the speed obtained in step S340 is within the specified speed (S350)

It is determined whether both the Trg # 1 signal, which is the first trigger signal generated in step S320, and the Trg # 2, which is the second trigger signal generated in step S350, are generated in step S360. In step S360, 1 signal and Trg # 2, which is the second trigger signal, are generated, the trigger is started and the velocity is measured.

In another embodiment of the present invention

When the movement sensing apparatus 100 according to the embodiment of the present invention is used singly while radiating the transmission frequency f ₀ at an arbitrary place, the movement sensing apparatus 100 can calculate the movement parameters of the moving object flying or moving Stable measurement is possible.

However, in the case where at least one movement sensing apparatus 100 is used while emitting a transmission frequency f ₀ in an arbitrary reference plane, among a plurality of movement sensing apparatuses emitting a transmission frequency f ₀ , If the distance between the movement detection device mutually equal to or smaller than the predetermined distance, the neighbor is any of the first transmitted frequency f _0, and a harmonic of the transmission frequency f ₀ emitted from the movement detection device arranged, adjacent to place any The first and second movement sensing devices may be caused to induce electromagnetic interference with each other and the radiation beam width of the antennas of any of the adjacently disposed first movement sensing devices may be different from that of any adjacent, The first and second movement sensing devices, which are adjacent to each other, can overlap the radiation beam width of the antenna, Body, whether the moving object launched from the front of any of the first movement detection device, a case may occur that can not be distinguished whether the moving object launched from any of the second motion sensing device.

As a result, any of the first and second movement detection devices disposed adjacent to each other may fail to stably measure the movement parameters such as the speed with respect to the moving moving object.

Accordingly, in another embodiment of the present invention, the transmission frequency output from the transmitter of the movement sensing apparatus 100 is divided into a first frequency, a second frequency, and a second frequency, which have a predetermined frequency interval, the n and configured to generate a frequency, which the mobile sensing device 100, in any location, the transmission frequency f ₀ by using only a plurality of mobile sensors, one or more for emitting at least one of a result, adjacent arrangement It is possible to solve the electromagnetic interference problem between the plurality of movement detecting devices and the measurement error due to overlapping of the radiation beam width.

To this end, when the movement sensing apparatus 100 generates a transmission frequency using a dielectric resonator (DRO), a frequency voltage controller is configured to change an output frequency of the dielectric resonator through a voltage change, Can be controlled through a signal processor in a predetermined voltage range.

In addition, when the movement sensing apparatus 100 generates a transmission frequency using a frequency synthesizer (PLL), a frequency controller is implemented so that the output frequency of the frequency synthesizer can be changed to a predetermined algorithm, May be configured to be controllable through a signal processor.

Therefore, even if a plurality of the motion sensing apparatuses 100 are used, which are spaced apart from the reference plane by a predetermined distance, a transmission frequency output from the dielectric resonator or the frequency synthesizer is divided into a first frequency, The second frequency, and the n-th frequency, and by setting the radiation frequency of any adjacent first movement sensing device and the radiation frequency of any second movement sensing device to be different from each other, Such as the velocity of the moving object, can be measured.

While the present invention has been particularly shown and described with reference to exemplary embodiments thereof, it is to be understood that the invention is not limited to the exemplary embodiments or constructions. You can understand that you can. Therefore, it should be understood that the above-described embodiments are to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than the foregoing description, All changes or modifications that come within the scope of the equivalent concept are to be construed as being included within the scope of the present invention.

The present invention relates to an apparatus and a method for controlling an altitude of a receiver,

Claims (14)

A transmitter and a transmitter for radiating an electromagnetic signal in a frequency band of X-band, K-band, or Ka-band to a moving object;
A receiving antenna and a receiver for receiving an electromagnetic signal reflected by the moving object and having a Doppler frequency shift;
A signal processor for calculating a moving parameter of the moving object from a signal input from the receiver; And
And a controller for controlling the signal input from the signal processor to be displayed. The method according to claim 1,
An acoustic receiver for receiving sound generated when the moving object starts to move; And a trigger generator for generating a trigger signal from the signal input from the sound receiver,
Wherein the reception antenna is a plurality of reception antennas including a sum reception antenna, an azimuth reception antenna, and an altitude reception antenna,
Wherein the receiver is a plurality of receivers including a sum receiver, an altitude angle receiver and an azimuth angle receiver, each of which is connected to the plurality of receiving antennas,
And the signal processor controls the transmitter according to the trigger signal. 3. The method of claim 2,
The transmitter includes a dielectric resonator for generating an electromagnetic signal of any one of the X-band, the K-band, and the Ka-band, a power amplifier for amplifying an electromagnetic signal generated in the dielectric resonator, A coupler for outputting a signal output from the antenna and a signal having the same frequency and the same power level for driving the mixers included in the plurality of receivers, and an isolator for inducing impedance matching between the transmission antenna and the power amplifier A device for detecting movement of an object. 3. The method of claim 2,
The signal processor includes an ADC, a RAM, a memory, and a DSP,
The ADC converts an analog Doppler signal processed by an analog Doppler signal and an analog trigger signal generated by the trigger generator into digital signals at the summation receiver, the azimuth angle receiver and the altitude receiver, and outputs an analog Doppler signal and a analog signal Converts the signals into digital Doppler signals and digital trigger signals, respectively, and transfers the signals to the RAM,
The RAM stores a digital Doppler signal and a digital trigger signal converted into a digital signal by the ADC,
Wherein the memory stores a signal processing program for calculating a movement parameter for an object to be processed in the DSP and data calculated in the signal processing program,
Wherein the DSP calculates a movement parameter of an object by using a signal processing program stored in the memory using a digital Doppler signal and a digital trigger signal stored in the RAM. The method of claim 3,
Further comprising a radiation beam controller for supplying driving power to the power amplifier, wherein the radiation beam controller causes the power amplifier to operate in a standby mode when there is no trigger signal detected by the trigger generator. The method of claim 3,
Further comprising a microwave switch disposed between the dielectric resonator and the power amplifier or between the power amplifier and the coupler, wherein the microwave switch is configured to switch the power amplifier to an object that causes the power amplifier to operate in the standby mode when there is no trigger signal detected by the trigger generator . The method according to claim 1,
The movement parameter includes at least one of movement of an object including at least one of a moving time, an initial moving speed, a moving angle, a moving speed, an acceleration, a moving distance, an altitude angle, an azimuth, a locus, a rotating speed, Sensing device. 3. The method of claim 2,
The trigger generator generates a first trigger signal when both the signal detected by the sound receiver and the Doppler signal input from the plurality of receivers are generated, and the signal processor calculates the velocity of the moving object from the Doppler signal And generates a second trigger signal to control the transmitter if the speed of the object is equal to or higher than a predetermined speed. The method of claim 3,
Wherein the transmitter is capable of varying the output transmission frequency. The method according to claim 1,
Wherein the signal processor extracts a line spectrum of an FM signal from an electromagnetic signal having a Doppler frequency shift reflected from an object moving while rotating, and calculates a rotation speed or a rotation frequency using the extracted FM signal. 11. The method of claim 10,
Wherein the signal processor comprises:
The analog Doppler signal is sampled at a predetermined sampling period and converted into a digital signal, a window function having a predetermined width is applied to a Doppler signal converted into a digital signal, and a fast Fourier transform is performed on N signals applied to the respective window functions The energy spectrum is obtained for each of the fast Fourier transformed signals, and the spectrum of the FM signal is extracted by calculating the energy spectrum on a two-dimensional plane of time-frequency. The Doppler line spectrum frequency f _d calculated, and the f _d to the center frequency to obtain the bandwidth BW _FM in the FM frequency line spectrum caused by a rotary motion, the center frequency from the plurality of line spectrum in the bandwidth f _d to the left, in the Yiwu symmetric random including the A peak value of a plurality of energy ray spectra is obtained, and the highest peak value among the obtained peak values Obtain an energy-ray spectrum signal having obtains binary highest peak Doppler line spectrum frequency signal is caused by the radial velocity V _r of the moving object while being rotated with the f _d or no matter or line spectrum of any of the side band signal, and for each signal arranged in the interval, calculated binary and the divided by the amplitude of the energy ray-spectrum signal having a high peak value, normalized, around the values of the normalized each Doppler line spectrum frequency f _d left, right order, etc. Order Bessel function stored in a reference table form with respect to each of the ordered normalized values and the obtained bandwidth BW _FM , and calculates an equation BW _FM = 2 x f _S x (? _FM +1) is applied to determine the rotational speed or the rotational frequency. 11. The method of claim 10,
Wherein the signal processor comprises:
An analog Doppler signal is sampled at a predetermined sampling period to be converted into a digital signal, a Doppler signal converted into a digital signal is subjected to a window function having a predetermined width, and a fast Fourier transform is performed on N signals applied to the respective window functions The energy spectrum of each signal obtained by the fast Fourier transform is obtained, and the spectrum of the FM signal is extracted by calculating the energy spectrum on the two-dimensional plane of the time-frequency. The energy spectrum signal obtained from the two- Doppler frequency due to the translational motion of the object f _d of the frequency and the line to obtain the energy of the spectrum, f with a random M-th line spectrum of the left and right sides by symmetrical about in the _d f _spM and f _spM 'of the frequency and the line obtaining a spectrum of the energy of the two frequencies obtained binary difference frequency _{Δf spM = | f spM -f spM} ' And obtaining a 2M number of line spectra existing in a symmetrical section and dividing the difference frequency? _{F spM} by the number of line spectra 2M to obtain a rotation speed or a rotation frequency. 13. The method according to claim 11 or 12,
Wherein the signal processor comprises:
An analog Doppler signal is sampled at a predetermined sampling period and converted into a digital signal. The time-series data converted into a digital signal is autocorrelated to obtain a line spectrum, wavelet decomposition is performed on the obtained line spectrum, An apparatus for detecting movement of an object for obtaining a frequency. 10. The method of claim 9,
Wherein the signal processor operates the frequency of the electromagnetic signal generated by the dielectric resonator or the frequency synthesizer at one of a plurality of predetermined operating frequencies.

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