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 saturationInfo
- 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- Withdrawn
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)
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)
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---|---|---|---|---|
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)
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 |
-
2018
- 2018-07-25 CN CN201810828031.4A patent/CN108710303B/en active Active
-
2019
- 2019-07-25 GB GB1910669.9A patent/GB2577593A/en not_active Withdrawn
Cited By (8)
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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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |