CN1570556A - Measuring device and method for spatial pose of rigid body - Google Patents

Measuring device and method for spatial pose of rigid body Download PDF

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CN1570556A
CN1570556A CN 200410009083 CN200410009083A CN1570556A CN 1570556 A CN1570556 A CN 1570556A CN 200410009083 CN200410009083 CN 200410009083 CN 200410009083 A CN200410009083 A CN 200410009083A CN 1570556 A CN1570556 A CN 1570556A
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CN1262816C (en
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段广洪
张辉
周潜
南仁东
王启明
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Tsinghua University
National Astronomical Observatories of CAS
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National Astronomical Observatories of CAS
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Abstract

刚体空间位姿测量装置及其测量方法,属于测控技术领域。为克服传统位姿测量装置的不足,本发明提出了一种接触式的低成本、高精度的刚体空间位姿测量装置,包括测量执行机构、数据采集装置以及存储计算程序的计算机;所述测量执行机构包括固定平台及固定在固定平台上的6个球铰,与运动刚体固连的运动平台及固定在运动平台上的6个球铰,两端分别与固定平台球铰和运动平台球铰相连的六个拉线式编码器。本发明还公开了一种刚体空间位姿测量方法,该方法根据上述测量装置获取的初始数据,利用迭代方程组得到被测刚体的空间位姿信息。本发明所述装置结构简单,系统实时性较高,能实现对被测刚体的全闭环实时控制。

Figure 200410009083

A rigid body space pose measuring device and a measuring method thereof belong to the technical field of measurement and control. In order to overcome the deficiencies of traditional pose measuring devices, the present invention proposes a contact-type low-cost, high-precision rigid body space pose measuring device, including a measurement actuator, a data acquisition device, and a computer storing a calculation program; the measurement The actuator includes a fixed platform and 6 spherical joints fixed on the fixed platform, a moving platform fixed to the moving rigid body and 6 spherical joints fixed on the moving platform, and the two ends are respectively connected to the fixed platform spherical hinge and the moving platform spherical hinge. Connected six wire-draw encoders. The invention also discloses a method for measuring the space pose of a rigid body. According to the initial data acquired by the measuring device, the method obtains the space pose information of the measured rigid body by using iterative equations. The device of the invention has simple structure, high real-time performance of the system, and can realize full-closed-loop real-time control of the rigid body to be tested.

Figure 200410009083

Description

Rigid space pose measuring apparatus and measuring method thereof
Technical field
The invention belongs to the observation and control technology field, relate to a kind of method and implement device that is used to measure rigid space six degree of freedom pose.
Background technology
In cartesian coordinate system, rigid body has six-freedom degree.In the Industry Control of lathe, mechanism, robot etc., in order to realize high-precision location, control can be adopted close-loop feedback control usually, and this has just proposed requirement to the kinetic measurement of spatial pose.In the close-loop feedback control that adopts, measure and mainly contain dual mode at present: the displacement (or angular displacement) in measurement topworks joint is fed back or the pose of direct measuring terminals feeds back.
In the scheme that measurement topworks's joint displacements (or angular displacement) is fed back, can be divided into two kinds of methods of semiclosed loop feedback and full cut-off ring feedback again.The displacement (or angular displacement) that the semiclosed loop feedback is only measured motor or leading screw, the kinematic train error after ignoring, the advantage of scheme is that cost is low, is convenient to realize that shortcoming is an error of having ignored machine driven system, precision is low; The displacement (or angular displacement) that full cut-off ring feedback needs to measure the practical set-up joint, instrument commonly used is a grating chi etc., and the advantage of this scheme is the precision height, and shortcoming is the cost height, and environment is had certain requirement.The common issue with that above-mentioned two kinds of schemes exist is, when tested rigid body pose was can not be whole controlled, this measurement scheme can't be finished measurement requirement.
Directly the method for measuring terminals pose normally adopts optical gauge to carry out non-contact measurement, as the positional information that adopts three optical instruments to measure three points on the rigid body can obtain the six degree of freedom posture information of rigid body.But common optical measuring apparatus real-time is poor, and the optical measuring apparatus can requirement of real time the time, cost becomes tens times increase again.Optical gauge has certain requirement to the space of environment and tested rigid body in addition.
The Stewart platform mechanism is the parallel institution that optimum is used for the implementation space six-freedom motion, it comes across nineteen sixties, general Stewart platform by a stationary platform, a motion platform and be connected in stationary platform and motion platform between six actuators form.By driving six actuators, make motion platform implementation space six-freedom motion.Present Stewart platform mechanism all is to be used for ACTIVE CONTROL.
Summary of the invention
The objective of the invention is to overcome the weak point of traditional location and attitude measuring, propose a kind of measurement mechanism and measuring method of low cost, high-precision rigid space position and attitude of contact.The present invention adopts the stay-supported scrambler to replace six actuators in the general Stewart platform mechanism, makes ACTIVE CONTROL become passive measurement, thereby obtains the posture information of tested motion rigid body.
Rigid space pose measuring apparatus disclosed by the invention is characterized in that: this measurement mechanism comprises the computing machine of measuring topworks, data collector and storage computation program; Described measurement topworks comprises a stationary platform and is fixed on 6 ball pivots on the described stationary platform, a motion platform that is connected with motion rigid body and be fixed on 6 ball pivots on the described motion platform, two ends respectively with stationary platform on six stay-supported scramblers linking to each other with 6 ball pivots on the motion platform of 6 ball pivots; Described data collector comprises six counters that link to each other with stay-supported scrambler output terminal respectively, the multiplexer that is connected with described each counter output, and the data transmit circuit that links to each other with described multiplexer; Described data transmit circuit is connected with described computing machine respective input mouth;
Described each ball pivot satisfies at the position coordinates of platform separately measures the Jacobian matrix J of topworks pConditional number smaller or equal to 10,
J p = l → 1 T ( Rp 1 × l → 1 ) T | p 1 | . . . . . . l → 6 T ( Rp 6 × l → 6 ) T | p 6 | ∈ R 6 × 6 ,
In the formula
Figure A20041000908300052
Be respectively along the vector of unit length on each stay-supported scrambler length direction, p 1~p 6Be the coordinate of 6 ball pivots in motion platform coordinate system p on the motion platform, R is the direction cosine battle array of motion platform coordinate system p about stationary platform coordinate system P, according to successively around the x of stationary platform coordinate system P, y, z axle anglec of rotation α, the Ka Erdan angle method for expressing of beta, gamma, the formula of embodying is:
R = cos β cos γ - cos β sin γ sin β sin α sin β cos γ + cos α sin γ - sin α sin β sin γ + cos α cos γ - sin α cos β - cos α sin β cos γ + sin α sin γ cos α cos β sin γ + sin α cos γ cos α cos β .
Of the present inventionly a kind ofly be improved to described 6 ball pivots that are fixed on the motion platform and directly be fixed on the motion rigid body, save described motion platform.
Stay-supported scrambler of the present invention is digital stay-supported scrambler.
It is of the present invention that a kind of to be improved to described stay-supported scrambler be analog stay-supported scrambler, this rigid space pose measuring apparatus also comprises an A/D capture card, the input end of described A/D capture card links to each other with the output terminal of described analog stay-supported scrambler, and output terminal links to each other with six counters respectively.
The invention also discloses a kind of described measurement mechanism and carry out the method for rigid space pose measurement, it is characterized in that: this measuring method comprises the steps:
1) system initialization is promptly determined the coordinate of each ball pivot in platform coordinate system separately, the initial length of stay-supported scrambler and the initial coordinate of tested rigid body in the stationary platform coordinate system, and import described computing machine;
2) when tested rigid motion, utilize data collector to gather the length variations signal of stay-supported scrambler, and be sent in the computing machine;
3) be the system of equations initial value with the initial coordinate of tested rigid body in the stationary platform coordinate system, the following iterative equation group of the program solution in the computing machine obtains the spatial attitude information and the positional information of tested rigid body:
L i-|R·p i+T-P i|=0,i=1,…,6;
Wherein, L 1~L 6Be the measurement length that 6 stay-supported scramblers obtain, P iBe the coordinate of 6 ball pivots in stationary platform coordinate system P on the stationary platform, p iBe the coordinate of 6 ball pivots in motion platform coordinate system p on the motion platform,
R is the direction cosine battle array of motion platform coordinate system p about stationary platform coordinate system P, has comprised spatial attitude information to be asked, T=[x y z] TBe the position of initial point in stationary platform coordinate system P of motion platform coordinate system p, comprised spatial positional information to be asked;
4) with the pose of current motion rigid body initial value, realize continuous coverage as the iterative equation group.
The present invention compares existing technology and has following advantage:
The first, apparatus of the present invention adopt the connected mode of Stewart mechanism, and implementation structure is simple.
The second, this device is directly measured the pose of tested rigid body, and the simultaneity factor real-time is higher, so can realize the full cut-off ring of tested rigid body is controlled in real time.
The 3rd, stay-supported scrambler cost is low, uses reliably, and precision can reach 1 micron, can satisfy the measurement requirement of general precision.
The 4th, by rational ball pivot choice of location, make mechanism relatively more responsive to attitude, measuring accuracy is improved.
The 5th, simple to operate during measurement, quick, not high to the space requirement of environment and tested rigid body, be applicable to multiple occasion.
Description of drawings
Fig. 1 is that the system of rigid space pose measuring apparatus of the present invention constitutes synoptic diagram.
Fig. 2 is the process flow diagram of rigid space pose measuring method.
Fig. 3 a is the structural principle block diagram of one embodiment of the present of invention.
Fig. 3 b is the structural principle block diagram of an alternative embodiment of the invention.
Embodiment
Specifically describe the measuring method and the measurement mechanism of motion rigid body pose of the present invention in conjunction with the accompanying drawings.
As described in Figure 1, rigid space pose measuring apparatus of the present invention comprises the computing machine of measuring topworks, data collector and storage computation program; Described measurement topworks comprises stationary platform 1, is installed in six ball pivots 101~106 on the stationary platform; Motion platform 2 is installed in six ball pivots 201~206 on the motion platform; Corresponding connection ball pivot 101~106 and 201~206 stay-supported scrambler 301~306; The input end of data collector 4 is connected with the output terminal of stay-supported scrambler, and the output terminal of data collector 4 is connected with the respective input mouth of computing machine 5.
Stationary platform 1 is used for installing six ball pivots 101~106, makes the ball pivot stationkeeping, sets up a changeless stationary platform coordinate system on stationary platform, accurately measures the coordinate of ball pivot 101~106 in the stationary platform coordinate system.In specific embodiment, the concrete form of stationary platform 1 can be flat board and also can be framed structure, and according to tested movement of Rigid Body scope and angle, stationary platform can be installed in the top or the below of motion rigid body.
Motion platform 2 is used for installing six ball pivots 201~206, and the motion rigid body of the other end and required measurement is connected simultaneously.On motion platform, set up a motion platform coordinate system, accurately measure the coordinate of ball pivot 201~206 in the motion platform coordinate system.When on the rigid body of required measurement when being easier to ball pivot is installed, can dispense motion platform 2, directly six ball pivots 201~206 are installed on the rigid body of required measurement, and on tested rigid body, set up the motion platform coordinate system.In the present embodiment because the less difficult installation ball pivot of tested rigid body area, so employing motion platform 2.
Each ball pivot is when the position of platform should make tested rigid body in range of movement separately, and the Jacobian matrix conditional number of measuring topworks meets the demands.Jacobian matrix is represented the position and attitude error amount of motion platform and the mapping relations between side chain error in length amount, and its conditional number has reflected designed mechanism ratio of precision on all directions in the space, is an important indicator weighing measuring accuracy.According to discovering, when the conditional number of Jacobian matrix greater than 10 the time, final measuring accuracy will sharply descend, and illustrate that the design of ball pivot coordinate is unreasonable, need redesign ball pivot position.The conditional number of the Jacobian matrix of the measurement topworks in the rigid space pose measuring apparatus of the present invention is smaller or equal to 10, preferably in 4~5.The formula that embodies of Jacobian matrix is:
J p = l → 1 T ( Rp 1 × l → 1 ) T | p 1 | . . . . . . l → 6 T ( Rp 6 × l → 6 ) T | p 6 | ∈ R 6 × 6 ,
In the formula
Figure A20041000908300072
Be respectively along the vector of unit length on each stay-supported scrambler length direction, p 1~p 6Be the coordinate of 6 ball pivots in motion platform coordinate system p on the motion platform, R is the direction cosine battle array of motion platform coordinate system p about stationary platform coordinate system P, according to successively around the x of stationary platform coordinate system P, y, z axle anglec of rotation α, the Ka Erdan angle method for expressing of beta, gamma, the formula of embodying is:
R = cos β cos γ - cos β sin γ sin β sin α sin β cos γ + cos α sin γ - sin α sin β sin γ + cos α cos γ - sin α cos β - cos α sin β cos γ + sin α sin γ cos α cos β sin γ + sin α cos γ cos α cos β .
Stay-supported scrambler 301~306, two ends link to each other with the motion platform ball pivot with the stationary platform ball pivot respectively, note the situation of length variations between corresponding ball pivot when tested rigid motion by scrambler.The form that data collector 4 becomes computing machine to receive the data-switching of stay-supported scrambler 301~306 is unifiedly resolved data transmission in the computing machine 5 of program to storing pose.
The stay-supported scrambler can be digital or analog on the output data mode.When adopting digital stay-supported scrambler, see Fig. 3 a, data collector 4 comprises the counter of six record coding device variable quantities, with six road signals merge into the multiplexer of one road signal and link to each other with multiplexer will converge after signal send to the data transmit circuit of computing machine.Digital stay-supported scrambler output terminal links to each other with six counters, and each counter output is connected with multiplexer, and data transmit circuit is connected with described computing machine respective input mouth.When adopting analog stay-supported scrambler, see Fig. 3 b, this rigid space pose measuring apparatus comprises that also one is the A/D capture card of digital signal with analog signal conversion, the input end of described A/D capture card links to each other with the output terminal of described analog stay-supported scrambler, and output terminal links to each other with six counters in the data collector 4 respectively.
The stay-supported scrambler is except that the way of output, aspect counting, specifically can adopt increment type or absolute type, on the circuit characteristic, can select voltage-type, current mode etc., in specific embodiment, can select encapsulation complete finished product stay-supported scrambler and multiplexer for use, as the digital increments formula voltage-type stay-supported scrambler HLS-M-1005 of HONTKO company, 74151 multiplexers etc.The data transmit circuit of data collector can be selected general serial ports transtation mission circuit, the receivable modes of computing machine such as parallel port transtation mission circuit for use.
Stored the computing machine 5 that pose resolves algorithm, the data and coordinate and 201~206 ball pivots the coordinate in motion platform coordinate system of ball pivot 101~106 in the stationary platform coordinate system of stay-supported scrambler are combined, by finding the solution position and the attitude that the motion of mechanism equation obtains motion platform relative fixed platform.
As shown in Figure 2.The flow process of rigid space pose measuring method of the present invention is as follows:
(1) system initialization: this part is mainly determined the parameter that is applied in the follow-up measurements and calculations, comprising ball pivot 101~106 and 201~206 coordinate in stationary platform coordinate system and motion platform coordinate system respectively, the initial length of stay-supported scrambler and be used under the tested rigid body initial situation of iterative equation coordinate at the stationary platform coordinate system, and with described coordinate input computing machine;
(2) data that the stay-supported scrambler is measured are transferred in the computing machine by data collector.If the stay-supported scrambler is increment type stay-supported scrambler, then need distance between ball pivot is respectively organized in the initial length addition of length variations amount in the stay-supported scrambler and stay-supported scrambler.
(3) find the solution locus and the spatial attitude that following iterative equation group obtains motion rigid body.
L i-|R·p i+T-P i|=0,i=1,…,6
T=[x y z in the formula] TBe the position of initial point in coordinate system P of coordinate system p, can obtain the spatial positional information of motion rigid body; R is the direction cosine battle array of motion platform coordinate system p about stationary platform coordinate system P, according to successively around the x of stationary platform coordinate system P, y, z axle limited angle rotating α, the Ka Erdan angle method for expressing of beta, gamma, the formula of embodying is:
R = cos β cos γ - cos β sin γ sin β sin α sin β cos γ + cos α sin γ - sin α sin β sin γ + cos α cos γ - sin α cos β - cos α sin β cos γ + sin α sin γ cos α cos β sin γ + sin α cos γ cos α cos β
L 1~L 6Be the measurement length that 6 stay-supported scramblers obtain.P iBe the coordinate of six ball pivots in stationary platform coordinate system P on the stationary platform.p iBe the coordinate of six ball pivots in motion platform coordinate system p on the motion platform.
In concrete enforcement, above-mentioned iterative equation group can adopt newton-La Feixunfa to find the solution.Below in order to express easily, this iterative algorithmic formula is described below:
Adopt newton-La Feixunfa to find the solution the method for Stewart kinematics of mechanism normal solution.
Motion of mechanism is just being solved an equation and can be expressed as:
f i(x,y,z,α,β,γ)=L i-|R·p i+T-P i|=0 i=1,2,…6
This system of equations is 6 nonlinear equations that contain 6 unknown numbers.Make X=(x, y, z, α, beta, gamma), F (X)=[f 1(X), f 2(X), f 3(X), f 4(X), f 5(X), f 6(X)] TX *Be solution of equations.Newton-La Feixunfa is an iterative algorithm.Equation Taylor is launched, obtains:
F(X+ΔX)=F(X)+JδX+O(δX 2)
J is the Jacobian matrix of equation in the formula, J ij = ∂ f i ∂ X j . Ignore the second order amount of equation, and make F that (X+ Δ X)=0 has:
JδX=-F(X)
This is a system of linear equations, separates the X=-J into δ -1F (X).Therefore its iterative process is: X New=X Old+ δ X.
(4) pose of current motion rigid body is substituted the initial value of iterative equation, prepare, realize continuous coverage for measure next time.

Claims (5)

1.刚体空间位姿测量装置,其特征在于:该测量装置包括测量执行机构、数据采集装置以及存储计算程序的计算机;所述测量执行机构包括一个固定平台及固定在所述固定平台上的6个球铰,一个与运动刚体固连的运动平台及固定在所述运动平台上的6个球铰,两端分别与固定平台上的6个球铰和运动平台上的6个球铰相连的六个拉线式编码器;所述数据采集装置包括分别与拉线式编码器输出端相连的六个计数器,与所述各计数器输出端连接的多路复用器,以及与所述多路复用器相连的数据发送电路;所述数据发送电路与所述计算机相应输入端口连接;1. Rigid body space pose measuring device is characterized in that: the measuring device comprises a measuring actuator, a data acquisition device and a computer storing a calculation program; the measuring actuator comprises a fixed platform and 6 fixed on the fixed platform a ball joint, a motion platform fixed to the motion rigid body and 6 ball joints fixed on the motion platform; Six wire-drawn encoders; the data acquisition device includes six counters connected to the output ends of the wire-drawn encoders respectively, a multiplexer connected to the output ends of the counters, and a multiplexer connected to the multiplexer A data transmission circuit connected to the device; the data transmission circuit is connected to the corresponding input port of the computer; 所述各球铰在各自平台的位置坐标满足测量执行机构雅克比矩阵Jp的条件数小于等于10,The position coordinates of the respective spherical joints on their respective platforms satisfy the condition number of the Jacobian matrix Jp of the measurement actuator being less than or equal to 10, JJ PP == ll →&Right Arrow; 11 TT (( RpRp 11 ×× ll →&Right Arrow; 11 )) TT || pp 11 || ·· ·&Center Dot; ·&Center Dot; ·&Center Dot; ·&Center Dot; ·&Center Dot; ll →&Right Arrow; 66 TT (( RpRp 66 ×× ll →&Right Arrow; 66 )) TT || pp 66 || ∈∈ RR 66 ×× 66 ,, 式中 分别是沿每个拉线式编码器长度方向上的单位向量,p1~p6是运动平台上的6个球铰在运动平台坐标系P中的坐标,R为运动平台坐标系P关于固定平台坐标系P的方向余弦阵,按照依次绕固定平台坐标系P的x,y,z轴旋转角度α,β,γ的卡尔丹角表示方法,具体表达式为:In the formula are the unit vectors along the length direction of each cable-guide encoder, p 1 ~ p 6 are the coordinates of the six spherical joints on the moving platform in the moving platform coordinate system P, and R is the moving platform coordinate system P with respect to the fixed platform The direction cosine matrix of the coordinate system P is expressed according to the Cardan angle representation method of rotating angles α, β, and γ around the x, y, and z axes of the fixed platform coordinate system P in turn, and the specific expression is: RR == coscos ββ coscos γγ -- coscos ββ sinsin γγ sinsin ββ sinsin αα sinsin ββ coscos γγ ++ coscos αα sinsin γγ -- sinsin αα sinsin ββ sinsin γγ ++ coscos αα coscos γγ -- sinsin αα coscos ββ -- coscos αα sinsin ββ coscos γγ ++ sinsin αα sinsin γγ coscos αα sinsin ββ sinsin γγ ++ sinsin αα coscos γγ coscos αα coscos ββ .. 2.根据权利要求1所述的刚体空间位姿测量装置,其特征在于:所述的固定在运动平台上的6个球铰直接固定在运动刚体上,省去所述运动平台。2. The rigid body space pose measurement device according to claim 1, characterized in that: the six spherical joints fixed on the moving platform are directly fixed on the moving rigid body, omitting the moving platform. 3.根据权利要求1或2所述的刚体空间位姿测量装置,其特征在于:所述拉线式编码器是数字式拉线式编码器。3. The rigid body space pose measurement device according to claim 1 or 2, characterized in that: the wire-guy encoder is a digital wire-guy encoder. 4.根据权利要求1或2所述的刚体空间位姿测量装置,其特征在于:所述拉线式编码器是模拟式拉线式编码器,该刚体空间位姿测量装置还包括一个A/D采集卡,所述A/D采集卡的输入端与所述模拟式拉线式编码器的输出端相连,输出端分别与六个计数器相连。4. The rigid body space pose measuring device according to claim 1 or 2, characterized in that: the cable-stayed encoder is an analog cable-stayed encoder, and the rigid-body space pose measuring device also includes an A/D acquisition card, the input end of the A/D acquisition card is connected to the output end of the analog pull wire encoder, and the output ends are respectively connected to six counters. 5.利用权利要求1所述测量装置进行刚体空间位姿测量的方法,其特征在于:该测量方法包括如下步骤:5. utilize the described measuring device of claim 1 to carry out the method for rigid body space pose measurement, it is characterized in that: this measuring method comprises the steps: 1)系统初始化,即确定各球铰在各自平台坐标系中的坐标,拉线式编码器的初始长度以及被测刚体在固定平台坐标系中的初始坐标,并输入所述计算机;1) System initialization, that is, determine the coordinates of each spherical joint in the respective platform coordinate system, the initial length of the cable encoder and the initial coordinates of the measured rigid body in the fixed platform coordinate system, and input them into the computer; 2)当被测刚体运动时,利用数据采集装置采集拉线式编码器的长度变化信号,并传送到计算机中;2) When the measured rigid body is moving, use the data acquisition device to collect the length change signal of the cable encoder and transmit it to the computer; 3)以被测刚体在固定平台坐标系中的初始坐标为方程组初始值,计算机中的程序求解下述迭代方程组,得到被测刚体的空间姿态信息及位置信息:3) Taking the initial coordinates of the measured rigid body in the fixed platform coordinate system as the initial value of the equations, the program in the computer solves the following iterative equations to obtain the spatial attitude information and position information of the measured rigid body: Li-|R·pi+T-Pi|=0,i=1,…,6;L i -|R · p i +TP i |=0, i=1,...,6; 其中,L1~L6为6个拉线式编码器得到的测量长度,Pi是固定平台上的6个球铰在固定平台坐标系P中的坐标,pi是运动平台上的6个球铰在运动平台坐标系p中的坐标,Among them, L 1 ~ L 6 are the measured lengths obtained by 6 wire-guide encoders, P i is the coordinates of the 6 spherical joints on the fixed platform in the coordinate system P of the fixed platform, and pi is the 6 ball joints on the moving platform The coordinates of the hinge in the motion platform coordinate system p, R为运动平台坐标系p关于固定平台坐标系P的方向余弦阵,包含了待求的空间姿态信息,T=[x y z]T是运动平台坐标系p的原点在固定平台坐标系P中的位置,包含了待求的空间位置信息;R is the direction cosine matrix of the moving platform coordinate system p with respect to the fixed platform coordinate system P, which contains the space attitude information to be sought, T=[x y z] T is the position of the origin of the moving platform coordinate system p in the fixed platform coordinate system P , which contains the requested spatial location information; 4)将当前运动刚体的位姿作为迭代方程组的初始值,实现连续测量。4) The pose of the current moving rigid body is used as the initial value of the iterative equations to realize continuous measurement.
CN 200410009083 2004-05-12 2004-05-12 Rigid body space pose measuring device and its measuring method Expired - Fee Related CN1262816C (en)

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CN110986919A (en) * 2019-12-24 2020-04-10 之江实验室 Pose/force testing device based on six-degree-of-freedom flexible parallel mechanism
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CN100492238C (en) * 2006-04-25 2009-05-27 中国科学院国家天文台南京天文光学技术研究所 Test method for three-bar modular attitude control mechanism
CN100447528C (en) * 2006-05-31 2008-12-31 中国科学院沈阳自动化研究所 Pose measuring plane sensor
CN100401010C (en) * 2006-08-25 2008-07-09 哈尔滨工业大学 Non-contact three-axis air bearing table rotation angle measurement device
CN100538277C (en) * 2007-06-08 2009-09-09 武汉钢铁(集团)公司 The pick-up unit of silicon steel rotary type annealing furnace furnace bed rotating distance and speed and method
CN101377812B (en) * 2008-07-11 2010-05-12 北京航空航天大学 Method for recognizing position and attitude of space plane object
CN101628174B (en) * 2009-08-18 2011-04-27 刘铮 Extraction method of table coordinates of snooker table with automatic distortion correction
WO2012129882A1 (en) * 2011-03-29 2012-10-04 长沙中联重工科技发展股份有限公司 Three-dimensional space vibration measuring device and method
CN102705429A (en) * 2012-04-12 2012-10-03 重庆大学 Method of damping vibration attenuation of six-freedom-degree space
CN102636139A (en) * 2012-04-12 2012-08-15 中国工程物理研究院激光聚变研究中心 Six-displacement-sensor dynamic measuring method of space six-degree-of-freedom movement
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CN102705429B (en) * 2012-04-12 2014-11-05 重庆大学 Method of damping vibration attenuation of six-freedom-degree space
CN102628728A (en) * 2012-04-12 2012-08-08 中国工程物理研究院激光聚变研究中心 Spatial six-degree-of-freedom vibration measuring and damping vibration attenuating method
CN104236629B (en) * 2014-09-17 2017-01-18 上海大学 Pull wire type measuring system and method applied to spatial location accuracy and track measurement of industrial robot
CN104236629A (en) * 2014-09-17 2014-12-24 上海大学 Pull wire type measuring system and method applied to spatial location accuracy and track measurement of industrial robot
CN104236543A (en) * 2014-09-17 2014-12-24 上海大学 Cable type measurement system and measurement method for industrial robot spatial pose precision and track measurement
CN104236543B (en) * 2014-09-17 2017-06-23 上海大学 For industrial robot spatial pose precision and the stay-supported measuring system and measuring method of trajectory measurement
CN104359445A (en) * 2014-11-13 2015-02-18 张得礼 Serial movement mechanism parameter error measuring device and method based on pull rope encoder
CN104359445B (en) * 2014-11-13 2018-02-09 南京航空航天大学 Serial kinematic mechanism parameter error measuring means and method based on drawstring encoder
CN104493808A (en) * 2014-11-26 2015-04-08 上海大学 System and method for pull-on-the-cable measurement of spatial pose precision and tracks of moving component
CN105043326B (en) * 2015-06-17 2017-12-19 浙江工商大学 A kind of intercity Freeway Transport goods displacement real-time detection apparatus
CN105043326A (en) * 2015-06-17 2015-11-11 浙江工商大学 Device for detecting displacement of cargo transported in intercity highway in real time
CN105444722B (en) * 2015-12-21 2018-05-01 中国科学院长春光学精密机械与物理研究所 The method of detection platform attitudes vibration
CN105444722A (en) * 2015-12-21 2016-03-30 中国科学院长春光学精密机械与物理研究所 Method for detecting changes of postures of platform
CN106654516A (en) * 2016-11-16 2017-05-10 上海卫星工程研究所 High-precision measuring device and high-precision measuring method suitable for multipoint distribution deployable antennas
CN106654516B (en) * 2016-11-16 2019-03-29 上海卫星工程研究所 High precision measuring device and method suitable for multiple spot distribution deployable antenna
CN108253996A (en) * 2016-12-28 2018-07-06 比亚迪股份有限公司 Bracing wire encoding measurement device, bracing wire space encoder location measurement method and system
CN108253996B (en) * 2016-12-28 2020-02-07 比亚迪股份有限公司 Guy wire code measuring device, guy wire code space position measuring method and system
CN110986919A (en) * 2019-12-24 2020-04-10 之江实验室 Pose/force testing device based on six-degree-of-freedom flexible parallel mechanism
CN113049147A (en) * 2019-12-26 2021-06-29 中国电力科学研究院有限公司 Tension monitoring device and method for overhead power transmission conductor
CN114952942A (en) * 2022-06-13 2022-08-30 南京工程学院 A robot pose measurement device and method based on six-wire encoder
CN118518314A (en) * 2024-07-25 2024-08-20 中国工程物理研究院总体工程研究所 Aerodynamic force testing method based on Stewart platform

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