GB201910669D0 - Method for controlling relative attitude of spacecrafts having multi-source disturbances and actuator saturation - Google Patents

Method for controlling relative attitude of spacecrafts having multi-source disturbances and actuator saturation

Info

Publication number
GB201910669D0
GB201910669D0 GBGB1910669.9A GB201910669A GB201910669D0 GB 201910669 D0 GB201910669 D0 GB 201910669D0 GB 201910669 A GB201910669 A GB 201910669A GB 201910669 D0 GB201910669 D0 GB 201910669D0
Authority
GB
United Kingdom
Prior art keywords
spacecrafts
relative attitude
controlling relative
actuator saturation
disturbances
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.)
Withdrawn
Application number
GBGB1910669.9A
Other versions
GB2577593A (en
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.)
Northwestern Polytechnical University
Original Assignee
Northwestern Polytechnical University
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 Northwestern Polytechnical University filed Critical Northwestern Polytechnical University
Publication of GB201910669D0 publication Critical patent/GB201910669D0/en
Publication of GB2577593A publication Critical patent/GB2577593A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B13/00—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion
    • G05B13/02—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric
    • G05B13/0265—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric the criterion being a learning criterion
    • G05B13/027—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric the criterion being a learning criterion using neural networks only
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/244—Spacecraft control systems
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/244—Spacecraft control systems
    • B64G1/245—Attitude control algorithms for spacecraft attitude control
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B64G1/646—Docking or rendezvous systems
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B13/00—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion
    • G05B13/02—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric
    • G05B13/04—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric involving the use of models or simulators
    • G05B13/042—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric involving the use of models or simulators in which a parameter or coefficient is automatically adjusted to optimise the performance

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Artificial Intelligence (AREA)
  • Radar, Positioning & Navigation (AREA)
  • General Physics & Mathematics (AREA)
  • Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Evolutionary Computation (AREA)
  • Software Systems (AREA)
  • Medical Informatics (AREA)
  • Computer Vision & Pattern Recognition (AREA)
  • Health & Medical Sciences (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
GB1910669.9A 2018-07-25 2019-07-25 Method for controlling relative attitude of spacecrafts having multi-source disturbances and actuator saturation Withdrawn GB2577593A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810828031.4A CN108710303B (en) 2018-07-25 2018-07-25 Spacecraft relative attitude control method containing multi-source disturbance and actuator saturation

Publications (2)

Publication Number Publication Date
GB201910669D0 true GB201910669D0 (en) 2019-09-11
GB2577593A GB2577593A (en) 2020-04-01

Family

ID=63874215

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1910669.9A Withdrawn GB2577593A (en) 2018-07-25 2019-07-25 Method for controlling relative attitude of spacecrafts having multi-source disturbances and actuator saturation

Country Status (2)

Country Link
CN (1) CN108710303B (en)
GB (1) GB2577593A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113485395A (en) * 2021-06-29 2021-10-08 北京控制工程研究所 Fixed time relative attitude and orbit tracking control method under error constraint
CN113625742A (en) * 2021-09-09 2021-11-09 哈尔滨理工大学 Spacecraft attitude tracking control algorithm
CN113961010A (en) * 2021-08-26 2022-01-21 中国科学院合肥物质科学研究院 Four-rotor plant protection unmanned aerial vehicle tracking control method based on anti-saturation finite time self-adaptive neural network fault-tolerant technology
CN114371618A (en) * 2021-12-15 2022-04-19 北京机电工程研究所 Extended state observer compensation method based on neural network and active disturbance rejection controller
CN117193356A (en) * 2023-09-05 2023-12-08 哈尔滨工业大学 Spacecraft formation preset time preset precision posture cooperative control method based on distributed state observer and control system thereof

Families Citing this family (16)

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CN109281894B (en) * 2018-10-29 2020-04-21 南京航空航天大学 Nonlinear compensation method for miniature volumetric remote control hydrostatic actuator
CN109739248B (en) * 2019-01-07 2021-08-03 大连海事大学 Ship-borne three-degree-of-freedom parallel stable platform stability control method based on ADRC
CN110134137B (en) * 2019-06-18 2021-11-23 哈尔滨工业大学（深圳） Spacecraft attitude tracking control method based on extended state observer
CN110456807B (en) * 2019-07-02 2021-01-12 西北工业大学 Multi-spacecraft consistency dynamic gain control method
CN111152225B (en) * 2020-01-15 2021-04-06 北京科技大学 Uncertain mechanical arm fixed time trajectory tracking control method with input saturation
CN111562793B (en) * 2020-04-08 2021-11-02 中南大学 Spacecraft attitude control method considering task time constraint
CN111474922B (en) * 2020-05-08 2021-07-16 哈尔滨工业大学 Method for constructing controller of continuous nonlinear system
CN111442786B (en) * 2020-05-21 2021-08-20 合肥工业大学 Zero drift deviation and attitude estimation method of aircraft gyroscope
CN112152539A (en) * 2020-09-29 2020-12-29 中国船舶重工集团公司第七二四研究所 Neural network compensation motor load moment observer implementation method
CN112363522B (en) * 2020-11-09 2022-09-27 西北工业大学 Networked spacecraft attitude control method based on hybrid forced observer
CN112731813B (en) * 2020-12-29 2022-05-13 西北工业大学 Spacecraft multi-source interference random model prediction control method based on composite disturbance observer
CN112882390B (en) * 2021-01-19 2022-05-20 杭州电子科技大学 Finite time output feedback control method for spacecraft rendezvous system
CN113619814B (en) * 2021-06-29 2023-06-06 北京控制工程研究所 Relative attitude and orbit coupling control method for final approaching section of intersection butt joint
CN114671050B (en) * 2022-03-30 2023-01-24 哈尔滨工业大学 Spacecraft tracking control method based on integrated linear operator and anti-saturation technology
CN114779799B (en) * 2022-05-23 2023-05-16 哈尔滨工业大学 Flexible spacecraft attitude and orbit tracking control method based on expansion disturbance observer
CN116627042B (en) * 2023-07-20 2023-09-29 南京邮电大学 Distributed collaborative tracking method for asymmetric saturated multi-self-body system of actuator

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102749852B (en) * 2012-07-24 2014-07-02 北京航空航天大学 Fault-tolerant anti-interference control method for multisource interference system
CN103235598B (en) * 2013-05-14 2016-08-10 北京理工大学 A kind of method adjusting thruster direction sensing assembly spacecraft centroid
CN103412571B (en) * 2013-07-22 2016-05-25 西北工业大学 A kind of spacecraft relative Attitude Control for Spacecraft method based on feedback linearization technology
CN103955224B (en) * 2014-04-22 2017-01-18 北京控制工程研究所 Attitude control method for relative motion visual line tracking
US9146557B1 (en) * 2014-04-23 2015-09-29 King Fahd University Of Petroleum And Minerals Adaptive control method for unmanned vehicle with slung load
CN104238357A (en) * 2014-08-21 2014-12-24 南京航空航天大学 Fault-tolerant sliding-mode control method for near-space vehicle
CN105843244A (en) * 2016-06-02 2016-08-10 北京航空航天大学 Output feedback-based flexible spacecraft precise attitude control method
CN108181920B (en) * 2018-01-31 2021-08-31 天津大学 High-precision attitude tracking control method for quad-rotor unmanned aerial vehicle based on given time

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113485395A (en) * 2021-06-29 2021-10-08 北京控制工程研究所 Fixed time relative attitude and orbit tracking control method under error constraint
CN113485395B (en) * 2021-06-29 2024-03-15 北京控制工程研究所 Relative pose track tracking control method for fixed time under error constraint
CN113961010A (en) * 2021-08-26 2022-01-21 中国科学院合肥物质科学研究院 Four-rotor plant protection unmanned aerial vehicle tracking control method based on anti-saturation finite time self-adaptive neural network fault-tolerant technology
CN113961010B (en) * 2021-08-26 2023-07-18 中国科学院合肥物质科学研究院 Tracking control method for four-rotor plant protection unmanned aerial vehicle
CN113625742A (en) * 2021-09-09 2021-11-09 哈尔滨理工大学 Spacecraft attitude tracking control algorithm
CN114371618A (en) * 2021-12-15 2022-04-19 北京机电工程研究所 Extended state observer compensation method based on neural network and active disturbance rejection controller
CN114371618B (en) * 2021-12-15 2023-11-03 北京机电工程研究所 Neural network-based extended state observer compensation method and active disturbance rejection controller
CN117193356A (en) * 2023-09-05 2023-12-08 哈尔滨工业大学 Spacecraft formation preset time preset precision posture cooperative control method based on distributed state observer and control system thereof

Also Published As

Publication number Publication date
CN108710303B (en) 2021-06-08
CN108710303A (en) 2018-10-26
GB2577593A (en) 2020-04-01

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