CN112033233A - Indirect drive high-precision servo implementation method under nonlinear interference - Google Patents

Indirect drive high-precision servo implementation method under nonlinear interference Download PDF

Info

Publication number
CN112033233A
CN112033233A CN202010732428.0A CN202010732428A CN112033233A CN 112033233 A CN112033233 A CN 112033233A CN 202010732428 A CN202010732428 A CN 202010732428A CN 112033233 A CN112033233 A CN 112033233A
Authority
CN
China
Prior art keywords
stable platform
frame
servo control
servo
system model
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CN202010732428.0A
Other languages
Chinese (zh)
Other versions
CN112033233B (en
Inventor
吴盼良
商美霞
佐大伟
常志英
武因峰
王禄禄
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hebei Hanguang Heavy Industry Ltd
Original Assignee
Hebei Hanguang Heavy Industry Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hebei Hanguang Heavy Industry Ltd filed Critical Hebei Hanguang Heavy Industry Ltd
Priority to CN202010732428.0A priority Critical patent/CN112033233B/en
Publication of CN112033233A publication Critical patent/CN112033233A/en
Application granted granted Critical
Publication of CN112033233B publication Critical patent/CN112033233B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/01Arrangements thereon for guidance or control

Abstract

The invention discloses a method for realizing indirect drive high-precision servo under nonlinear interference, which belongs to the technical field of seeker stabilized platforms and can solve the problem of poor servo performance caused by nonlinear interference torque, gear drive backlash, friction torque and other factors caused by a through-axis cable. The through-axis cable adopted by the stable platform is in a spiral wiring mode; the method comprises the following steps: and constructing an ideal system model of the stable platform, and calibrating the ideal system model to obtain a transfer function G0 of the ideal system model. And performing servo control on a stable platform of the seeker by adopting a servo control algorithm, comparing the angular velocity v of the frame with the polarity of the output voltage u of the motor, and superposing backlash compensation in the control quantity calculated by the servo control algorithm when the polarities of v and u are different. And (3) performing superposition interference compensation d on the control quantity calculated by the servo control algorithm according to the difference e between the input quantity and the output quantity of the stable platform.

Description

Indirect drive high-precision servo implementation method under nonlinear interference
Technical Field
The invention relates to the technical field of seeker stabilization platforms, in particular to an indirect drive high-precision servo implementation method under nonlinear interference.
Background
The seeker is used as a key component of a guided weapon and comprises a stable platform, a target detector camera, a thermal infrared imager, a radar, a laser and the like and a target tracker. The stable platform is used as a part of the seeker, bears various optical and radar sensors, isolates external disturbance, ensures that the detector has clear imaging and the tracker has stable tracking. Meanwhile, a servo mechanism of the stable platform can quickly respond to the received instruction, and timely searching or target pointing is ensured. With the continuous progress of the technology and the more complex application environment, the seeker is developed towards miniaturization and compounding. The requirement for a stable platform is higher, and the miniaturization generally leads the stable platform to abandon a motor direct drive structure and use indirect drive instead; the composite structure leads signal lines in the platform to be increased, a large number of cables, particularly coaxial cables, penetrate through the servo rotating shaft, nonlinear interference torque caused by friction and deformation is increased, and challenges are brought to the realization of precision and stable indexes of a servo system.
The stabilized platform is to achieve isolation of disturbance and pointing targets, and is to be capable of moving in at least both horizontal and vertical directions, i.e. it comprises at least two mutually orthogonal frames, called azimuth frame and pitch frame. The azimuth frame bears various target detectors, the azimuth motor drives the azimuth frame to rotate horizontally, and the rotating angle and the rotating angular speed of the frame are measured by the azimuth rotary transformer and the azimuth gyroscope. The angle measured by the azimuth code disc is the azimuth frame angle. The whole azimuth frame is used as a load and is arranged on a rotating shaft of the pitching frame, and the pitching motor adopts a gear transmission mode to indirectly drive the load due to large load inertia and limited space. The pitching frame is also provided with a pitching rotary transformer for measuring the angle and a pitching gyroscope for measuring the angular speed. The azimuth motor, the azimuth rotary transformer, the azimuth gyroscope, the pitching voltage, the pitching rotary transformer and the pitching gyroscope are all connected to the servo circuit board through cables, closed-loop operation is carried out through a servo control algorithm in the processing chip, and the servo function of the stable platform is achieved. The servo circuit board is installed on the stable platform base, and the cables of the motor, the rotary transformer and the gyroscope of the azimuth frame can be connected to the servo circuit board only by penetrating through the pitching frame shaft. And the target detector carried in the azimuth frame can be connected to the target tracker on the base of the stable platform only by passing through the azimuth axis and the pitching axis. Usually, the signal cable of the target probe is a rigid coaxial cable, which generates a large elastic and frictional disturbing torque.
Therefore, how to implement a servo stabilization platform with high precision and strong robustness under nonlinear interference and indirect driving is a problem to be solved urgently at present.
Disclosure of Invention
In view of the above, the invention provides a method for implementing indirect drive high-precision servo under nonlinear interference, which can solve the problem of poor servo performance caused by nonlinear interference torque caused by a through-axis cable, gear transmission backlash, friction torque and other factors.
In order to achieve the purpose, the technical scheme of the invention is as follows: a high-precision servo implementation method of indirect drive under nonlinear interference is used for servo control of a stable platform of a seeker, wherein the stable platform comprises a motor, a frame and a gear drive structure, the gear drive structure comprises a drive end gear and a load end gear which are meshed with each other, the drive end gear is sleeved on an output shaft of the motor, the load end gear is sleeved on a drive shaft of the frame, and a shaft penetrating cable adopted by the stable platform is in a spiral wiring mode; the method comprises the following steps:
constructing an ideal system model of a stable platform, which specifically comprises the following steps: and taking out the shaft penetrating cable in the stable platform, adopting an external connection mode to replace a shaft penetrating connection mode, and directly connecting an output shaft of the motor with a driving shaft of the frame to realize direct drive of the frame.
And calibrating the ideal system model to obtain the transfer function G0 of the ideal system model.
Performing servo control on a stable platform of the seeker by adopting a servo control algorithm, comparing the angular velocity v of the frame with the polarity of the output voltage u of the motor, and when the polarities of v and u are different, superposing null return compensation in the control quantity calculated by the servo control algorithm, wherein the value of the null return compensation is kXu, and k is a preset adjustable parameter; when v and u have the same polarity, the backlash compensation is set to 0.
The control quantity calculated by the servo control algorithm is subjected to superposition interference compensation d according to the difference e between the input quantity and the output quantity of the stable platform;
and (4) setting.
Figure BDA0002603674940000031
Where H is the inverse of the transfer function G0; a is a set first adjustable parameter; b is a set second adjustable parameter; c is a set third adjustable parameter; t is a set fourth adjustable parameter; e1 is setting a first threshold; e2 is a set second adjustable threshold, e2 is less than e 1; s is the complex variable of the transfer function G0.
Further, the through-axis cable that the stable platform adopted specifically is for spiral wiring mode:
the rotating shaft is circumferentially provided with a movable inner baffle, and the movable inner baffle is provided with an opening for cable routing; the movable outer baffle is arranged on the outer ring of the movable inner baffle, and an opening at one side of the movable outer baffle is connected with the fixed frame; a smooth area between the movable outer baffle and the movable inner baffle is a wire groove; the cable passes through the opening on the movable inner baffle after passing through the rotating shaft, and passes through the fixing clamp for fixing after winding the movable inner baffle for a circle.
Has the advantages that:
the invention provides a method for realizing indirect drive high-precision servo under nonlinear interference, which comprises the steps of through-axis cable layout, ideal system model calibration, gear backlash compensation and interference segmented compensation. The deformation mode of the cable is fixed and dispersed through spiral wiring, so that the change of the nonlinear moment is easier to predict, the moment is reduced, and the problem of nonlinear disturbance moment caused by the shaft penetrating cable is solved. Meanwhile, the problem of poor servo performance caused by factors such as gear transmission backlash, friction torque and the like can be solved through gear backlash compensation and interference sectional compensation.
Drawings
Fig. 1 is a flowchart of an indirect drive high-precision servo implementation method under nonlinear interference according to an embodiment of the present invention;
FIG. 2 is a schematic diagram of spiral wiring according to an embodiment of the present invention; wherein, 1 is a rotating shaft, 2 is a movable inner baffle, 3 is a cable, 4 is an outer baffle, 5 is a fixed clamp, and a wire groove is arranged in the area between 2 and 4;
fig. 3 is a schematic diagram of a cable state at a limited angle of the rotating shaft during spiral wiring in the embodiment of the invention.
Detailed Description
The invention is described in detail below by way of example with reference to the accompanying drawings.
The invention provides a method for realizing indirect drive high-precision servo under nonlinear interference, which is used for carrying out servo control on a stable platform of a seeker, wherein the stable platform comprises a motor, a frame and a gear drive structure, the gear drive structure comprises a drive end gear and a load end gear which are meshed, the drive end gear is sleeved on an output shaft of the motor, and the load end gear is sleeved on a drive shaft of the frame; and the flow of the method is shown in figure 1, and comprises the following steps:
constructing an ideal system model of a stable platform, which specifically comprises the following steps: and taking out the shaft penetrating cable in the stable platform, adopting an external connection mode to replace a shaft penetrating connection mode, and directly connecting an output shaft of the motor with a driving shaft of the frame to realize direct drive of the frame.
And calibrating the ideal system model to obtain the transfer function G0 of the ideal system model.
Performing servo control on a stable platform of the seeker by adopting a servo control algorithm, comparing the angular velocity v of the frame with the polarity of the output voltage u of the motor, and when the polarities of v and u are different, superposing null return compensation in the control quantity calculated by the servo control algorithm, wherein the value of the null return compensation is kXu, and k is a preset adjustable parameter; when v and u have the same polarity, the backlash compensation is set to 0.
And (3) performing superposition interference compensation d on the control quantity calculated by the servo control algorithm according to the difference e between the input quantity and the output quantity of the stable platform.
And (4) setting.
Figure BDA0002603674940000051
Where H is the inverse of the transfer function G0; a is a set first adjustable parameter; b is a set second adjustable parameter; c is a set third adjustable parameter; t is a set fourth adjustable parameter; e1 is setting a first threshold; e2 is a set second adjustable threshold, e2 is less than e 1; s is the complex variable of the transfer function G0. Wherein a, b, c, T, e1 and e2 are set empirically, and the value that optimizes the compensation effect can be selected according to the final compensation effect.
The through-axis cable adopted by the stable platform is in a spiral wiring mode; as shown in fig. 2 and 3.
The rotating shaft 1 is provided with a movable inner baffle 2 along the circumferential direction, and the movable inner baffle 2 is provided with an opening for cable routing; the movable outer baffle 4 is arranged on the outer ring of the movable inner baffle 2, and an opening at one side of the movable outer baffle 4 is connected with the fixed frame 5; a smooth area between the movable outer baffle 4 and the movable inner baffle 2 is a wire groove; the cable passes through the opening on the movable inner baffle 2 after passing through the rotating shaft 1, and passes through the fixing clamp 5 for fixing after winding the movable inner baffle 2 for a circle.
In summary, the above description is only a preferred embodiment of the present invention, and is not intended to limit the scope of the present invention. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims (2)

1. An indirect drive high-precision servo realization method under nonlinear interference is used for carrying out servo control on a stable platform of a seeker, wherein the stable platform comprises a motor, a frame and a gear drive structure, the gear drive structure comprises a drive end gear and a load end gear which are meshed with each other, the drive end gear is sleeved on an output shaft of the motor, and the load end gear is sleeved on a drive shaft of the frame; and the method comprises the following steps:
constructing an ideal system model of the stable platform, which specifically comprises the following steps: taking out the shaft penetrating cable in the stable platform, adopting an external connection mode to replace a shaft penetrating connection mode, and directly connecting an output shaft of the motor with a driving shaft of the frame to realize direct drive of the frame;
calibrating the ideal system model to obtain a transfer function G0 of the ideal system model;
performing servo control on a stable platform of the seeker by adopting a servo control algorithm, comparing the angular velocity v of the frame with the polarity of the output voltage u of the motor, and when the polarities of v and u are different, superposing null return compensation in a control quantity calculated by the servo control algorithm, wherein the value of the null return compensation is kXu, and k is a preset adjustable parameter; when the polarities of v and u are the same, setting the backlash compensation to be 0;
the control quantity calculated by the servo control algorithm is subjected to superposition interference compensation d according to the difference e between the input quantity and the output quantity of the stable platform;
and (4) setting.
Figure FDA0002603674930000011
Where H is the inverse of the transfer function G0; a is a set first adjustable parameter; b is a set second adjustable parameter; c is a set third adjustable parameter; t is a set fourth adjustable parameter; e1 is setting a first threshold; e2 is a set second adjustable threshold, e2 is less than e 1; s is the complex variable of the transfer function G0.
2. The method of claim 1, wherein the through-axis cables used by the stabilization platform are routed in a spiral manner;
the rotating shaft (1) is provided with a movable inner baffle (2) along the circumferential direction, and the movable inner baffle (2) is provided with an opening for cable routing;
the movable outer baffle (4) is arranged on the outer ring of the movable inner baffle (2), and an opening at one side of the movable outer baffle (4) is connected with the fixed frame (5); a smooth area between the movable outer baffle (4) and the movable inner baffle (2) is a wire groove;
the cable passes through the rotating shaft (1), then is routed through an opening in the movable inner baffle (2), and then passes through the fixing clamp (5) for fixing after winding the movable inner baffle (2) for a circle.
CN202010732428.0A 2020-07-27 2020-07-27 Indirect driving high-precision servo implementation method under nonlinear interference Active CN112033233B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202010732428.0A CN112033233B (en) 2020-07-27 2020-07-27 Indirect driving high-precision servo implementation method under nonlinear interference

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202010732428.0A CN112033233B (en) 2020-07-27 2020-07-27 Indirect driving high-precision servo implementation method under nonlinear interference

Publications (2)

Publication Number Publication Date
CN112033233A true CN112033233A (en) 2020-12-04
CN112033233B CN112033233B (en) 2022-07-26

Family

ID=73583256

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202010732428.0A Active CN112033233B (en) 2020-07-27 2020-07-27 Indirect driving high-precision servo implementation method under nonlinear interference

Country Status (1)

Country Link
CN (1) CN112033233B (en)

Citations (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2253722A (en) * 1987-09-23 1992-09-16 Gen Electric Co Plc Stabilising arrangement
US5274314A (en) * 1993-02-12 1993-12-28 Texas Instruments Incorporated Adaptive friction compensator
US5369345A (en) * 1992-03-31 1994-11-29 Seagate Technology, Inc. Method and apparatus for adaptive control
JPH09258830A (en) * 1996-03-19 1997-10-03 Yaskawa Electric Corp Backlash suppression control method for position control
JP2006195566A (en) * 2005-01-11 2006-07-27 Yaskawa Electric Corp Servo control unit and control method therefor
CN1974325A (en) * 2006-12-14 2007-06-06 北京航空航天大学 Servo control system of magnetically suspended control moment gyroscope frame with precise friction compensation
US20130069581A1 (en) * 2011-09-19 2013-03-21 Samsung Techwin Co., Ltd. Control system for rotating shaft
CN103149948A (en) * 2013-02-04 2013-06-12 北京航空航天大学 Two-freedom-degree heavy-load tracking stabilized platform system
CN103344243A (en) * 2013-07-02 2013-10-09 北京航空航天大学 Friction parameter identification method for aerial remote-sensing inertial stabilization platform
CN103693205A (en) * 2013-12-30 2014-04-02 广东电网公司电力科学研究院 Pod stabilized platform control method based on backlash estimation and compensation
CN104460704A (en) * 2014-12-15 2015-03-25 南京理工大学 Tracking control method for pitching position of electric rotary table based on perturbation upper bound estimation
CN104808699A (en) * 2015-04-13 2015-07-29 武汉华中天勤光电系统有限公司 Servo control method based on gear mechanism
CN104965413A (en) * 2015-06-29 2015-10-07 南京理工大学 Friction compensation adaptive control method for controlled emission platform
CN105786024A (en) * 2016-03-02 2016-07-20 北京航空航天大学 Airborne photoelectric platform high precision tracking controller based on model error compensation and tracking control method thereof
CN107621783A (en) * 2017-08-26 2018-01-23 南京理工大学 Flat pad adaptive robust control method based on friciton compensation
CN109884881A (en) * 2018-06-13 2019-06-14 南京理工大学 A kind of design for surely taking aim at servo controller based on nonlinear PID controller technology
CN111338391A (en) * 2020-05-19 2020-06-26 北京中星时代科技有限公司 Two-axis four-frame photoelectric turntable control system

Patent Citations (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2253722A (en) * 1987-09-23 1992-09-16 Gen Electric Co Plc Stabilising arrangement
US5369345A (en) * 1992-03-31 1994-11-29 Seagate Technology, Inc. Method and apparatus for adaptive control
US5274314A (en) * 1993-02-12 1993-12-28 Texas Instruments Incorporated Adaptive friction compensator
JPH09258830A (en) * 1996-03-19 1997-10-03 Yaskawa Electric Corp Backlash suppression control method for position control
JP2006195566A (en) * 2005-01-11 2006-07-27 Yaskawa Electric Corp Servo control unit and control method therefor
CN1974325A (en) * 2006-12-14 2007-06-06 北京航空航天大学 Servo control system of magnetically suspended control moment gyroscope frame with precise friction compensation
US20130069581A1 (en) * 2011-09-19 2013-03-21 Samsung Techwin Co., Ltd. Control system for rotating shaft
CN103149948A (en) * 2013-02-04 2013-06-12 北京航空航天大学 Two-freedom-degree heavy-load tracking stabilized platform system
CN103344243A (en) * 2013-07-02 2013-10-09 北京航空航天大学 Friction parameter identification method for aerial remote-sensing inertial stabilization platform
CN103693205A (en) * 2013-12-30 2014-04-02 广东电网公司电力科学研究院 Pod stabilized platform control method based on backlash estimation and compensation
CN104460704A (en) * 2014-12-15 2015-03-25 南京理工大学 Tracking control method for pitching position of electric rotary table based on perturbation upper bound estimation
CN104808699A (en) * 2015-04-13 2015-07-29 武汉华中天勤光电系统有限公司 Servo control method based on gear mechanism
CN104965413A (en) * 2015-06-29 2015-10-07 南京理工大学 Friction compensation adaptive control method for controlled emission platform
CN105786024A (en) * 2016-03-02 2016-07-20 北京航空航天大学 Airborne photoelectric platform high precision tracking controller based on model error compensation and tracking control method thereof
CN107621783A (en) * 2017-08-26 2018-01-23 南京理工大学 Flat pad adaptive robust control method based on friciton compensation
CN109884881A (en) * 2018-06-13 2019-06-14 南京理工大学 A kind of design for surely taking aim at servo controller based on nonlinear PID controller technology
CN111338391A (en) * 2020-05-19 2020-06-26 北京中星时代科技有限公司 Two-axis four-frame photoelectric turntable control system

Also Published As

Publication number Publication date
CN112033233B (en) 2022-07-26

Similar Documents

Publication Publication Date Title
Masten Inertially stabilized platforms for optical imaging systems
CN108919841B (en) Composite shaft control method and system of photoelectric tracking system
CN110361829B (en) Telescope pointing error correction method and telescope
JP4982407B2 (en) Mobile object image tracking apparatus and method
Juqing et al. Precision laser tracking servo control system for moving target position measurement
CN113513952B (en) Electric steering engine, electric steering engine zero calibration method, device and storage medium
CN106802672B (en) A kind of real-time closed-loop tracking based on rotation biprism
JP2009115621A (en) Mobile image tracking device
CN112653367B (en) Control system and method for common rotating table
CN109597092A (en) A kind of space high precision photoelectric pointing system using complex controll
CN112683112A (en) Optical platform and radar co-frame turntable system
CN106502277A (en) Three-axis air-bearing table superhigh precision measurement apparatus and method based on tracking technique
CN212556849U (en) High-precision double-shaft simulation turntable with no shielding of clearance of pitching shaft
CN109884791B (en) Rapid high-precision scanning method based on rotating biprism
Ansari et al. Fast steering and quick positioning of large field-of-regard, two-axis, four-gimbaled sight
CN112033233B (en) Indirect driving high-precision servo implementation method under nonlinear interference
CN1007803B (en) Pointing compensation system for spacecraft instruments
CN108375997B (en) Orthogonality compensation method for two-axis servo control system of vehicle-mounted photoelectric observing and aiming system
CN102662407B (en) Tracking control method of three-axis telescope
Borrello A multi stage pointing acquisition and tracking (PAT) control system approach for air to air laser communications
CN113359871B (en) Fixed-point closed-loop method based on double-prism rotating device
CN104457816A (en) Optical telescope rotary encoder absolute position reference point calibration method
CN112319387B (en) Stay wire control type following stable platform
CN112165578B (en) Exposure compensation method for flight shooting
Xie et al. Research on optimal control strategy for velocity stability of space two-dimensional tracking turntable

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant