JPH05107000A - Controlling system for missile - Google Patents

Abstract

PURPOSE:To eliminate an attitude control unit in a missile by necessarily calculating an attitude control of the missile at a control unit side for controlling the flying attitude of the missile. CONSTITUTION:Attitude angle data to be transmitted from a missile through a radio wave 8 is displayed on a display panel 4 of a control unit 1 on the ground, and sent to an attitude control calculator 6. On the other hand, a command from a controller for operating the control unit 1 is also sent to the calculator 6 through a command panel 5. Then, the calculator 6 calculates based on the command from the controller and the attitude angle data of the missile, decides a steering amount (control amount) of the missile, and further sends the steering amount to the missile. Thus, the attitude control calculation is conducted in the control unit, thereby eliminating necessity of placing the attitude control unit in the missile.

Description

Detailed Description of the Invention

[0001]

BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a flying object control system, and more particularly to a flying object control method for remotely controlling a flying object such as a target unmanned airplane from the ground, onboard or on board by radio.

[0002]

2. Description of the Related Art A conventional unmanned aerial vehicle control system is shown in FIGS.

FIG. 3 shows the relationship between the ground control device 15 and the flying vehicle 9. The control device 15 has an antenna 2 that receives data transmitted from a flying object via a radio wave 7, and changes by time when the radio wave 7 emitted from a flying object 9 is captured and followed by the antenna 2. It tracks and monitors the position and attitude of flying objects.

On the other hand, a controller (pilot) operating the control device 15 monitors the position, attitude, etc. of the flying object displayed on the control device 1, and issues a command to the flying object 9 based on these information. It is decided that the flying body 9 is remotely controlled by the radio wave 8.

FIG. 4 is a diagram showing a remotely controlled flying object.

The flying body 9 is provided with an antenna 13 and a transceiver 10 for transmitting and receiving radio waves to and from the control device. Command data received from the control device 1 from the control device 1 is transmitted to the attitude control device 14. Sent to. The attitude control device 14 performs a predetermined calculation based on the attitude of the own aircraft and the command of the control device sent from the attitude sensor 11 mounted on the flying body 9 at a time and time, and the calculation result is obtained. The steering amount is determined from the above, and the posture control is performed by operating the steering mechanism 12.

[0007]

In this conventional flying object control system, since the attitude control of the flying object is performed by the attitude control device mounted on the flying object, a control device is required for each flying object. There is a drawback.

In particular, in the case of a flying object that is heavily worn such as a wireless target landing, the control device is also worn along with the flying object, which is a drawback in that it is a heavy economical burden.

An object of the present invention is to eliminate the above-mentioned drawbacks and to provide a flying body control method capable of controlling the flying posture of a flying body without mounting the posture control device for each flying body. It is in.

[0010]

According to the method of the present invention, in a control system of a flying object which is remotely controlled by radio, the attitude angle data of the flying object transmitted from the flying object is received, and based on the attitude angle data. It is configured to include means for calculating a control amount for controlling the flying attitude of the flying object and remotely controlling the flying object by radio based on the calculation result.

[0011]

DESCRIPTION OF THE PREFERRED EMBODIMENTS Next, the present invention will be described with reference to the drawings.

FIG. 1 is a block diagram of a flight control device according to an embodiment of the present invention. In the control device 1 shown in FIG. 1, the radio wave 7 transmitted from the flying object is captured by the antenna 2 and the transceiver 3 to track the position of the flying object which changes with time.

Further, the attitude angle data of the flying object transmitted via the radio wave 7 is displayed on the display panel 4 from the transceiver 3 together with the position data of the flying object.

On the other hand, the controller (pilot) arranged in the control device 1 determines a command to the flying object based on the position and attitude data of the flying object displayed on the display panel 4. This command amount is sent to the attitude control calculation device 6 via the command panel 5. Next, the attitude control calculation device 6 performs a predetermined calculation based on the attitude angle data of the flying object and the command amount, determines the steering amount (control amount) of the flying object, and transmits it via the radio wave 8 and the antenna 13. Sent to the flying body.

FIG. 2 is a configuration diagram of a flying object that is remotely controlled by the flying object control apparatus 1 of the present invention.

In the flying body 9, the attitude data measured by the attitude sensor 11 is transmitted via the transceiver 10 to the control device 1
Send to.

Further, the steering amount (control amount) of the flying object, which is transmitted from the control device 1 and received by the flying object transceiver 10, is
It is transmitted to the steering mechanism 12 of the flying object to operate the rudder.

In this manner, the flying body side does not need a computing device relating to the attitude control, and the attitude control can be performed only by the computation in the control device.

[0019]

As described above, according to the present invention, by performing the attitude control calculation of the flying object in the control device, the flying object does not need the attitude controlling apparatus, and the economical burden on the flying object is reduced. Has the effect of

[Brief description of drawings]

FIG. 1 is a configuration diagram of a control device for a flying object according to an embodiment of the present invention.

FIG. 2 is a configuration diagram of a flying object that is remotely steered by the control device of FIG.

FIG. 3 is a configuration diagram showing a relationship between a conventional control device and a flying object.

FIG. 4 is a configuration diagram of a flying object that is remotely controlled by a conventional control device.

[Explanation of symbols]

 DESCRIPTION OF SYMBOLS 1 Control device 2 Antenna 3 Transceiver 4 Display panel 5 Command pulse 6 Attitude control computing device 7 Radio wave 8 Radio wave 9 Flying object 10 Transmitter / receiver for flying object 11 Attitude sensor 12 Steering mechanism 13 Antenna 14 Attitude control device 15 Control device

Claims (1)

[Claims] 1. A control system for receiving a flying body attitude angle data transmitted from a flying body and controlling a flying attitude of the flying body based on the attitude angle data in a wireless remote control flying vehicle control system. A control system for a flying object, comprising means for calculating an amount and remotely controlling the flying object by radio based on the calculation result.