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A spatial non-cooperative target approach method based on predictive pursuit-flight game control

A non-cooperative target and space technology, which is applied in the field of tracking spacecraft orbit control based on the game of chasing and fleeing, can solve problems such as not considering control constraints, and achieve the effect of improving robustness and simple calculation

Active Publication Date: 2022-07-26
RES & DEV INST OF NORTHWESTERN POLYTECHNICAL UNIV IN SHENZHEN +1
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Problems solved by technology

also does not take into account the control constraints

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  • A spatial non-cooperative target approach method based on predictive pursuit-flight game control
  • A spatial non-cooperative target approach method based on predictive pursuit-flight game control
  • A spatial non-cooperative target approach method based on predictive pursuit-flight game control

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Embodiment Construction

[0043] The invention is mainly aimed at the space non-cooperative target with orbital maneuverability, and the tracking spacecraft and its approach problem are modeled as a pursuit and flight game problem between the target and the tracking spacecraft. Under the orbital coordinate system of the tracking spacecraft, a relative motion model is established; based on the model predictive control method, a discrete game model in the prediction time domain is obtained, and it is summarized as a maximum-minimum optimization with dynamic constraints and control constraints Problem; in the case of unknown target maneuvering strategy, the tracking spacecraft can improve the accuracy of target behavior prediction and the effect of target tracking by iteratively solving the optimal trajectory of the target and the corresponding maneuvering strategy.

[0044] The design steps of the space non-cooperative target approach method based on the prediction pursuit and escape game control of the p...

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Abstract

The invention provides a space non-cooperative target approach method based on predictive pursuit and escape game control. For the space non-cooperative target with orbital maneuverability, the tracking spacecraft and its approach problem are modeled as the pursuit between the target and the tracking spacecraft. Escape game problem. Under the orbital coordinate system of the tracking spacecraft, a relative motion model is established; based on the model predictive control method, a discrete game model in the prediction time domain is obtained, and it is summarized as a maximum-minimum optimization problem with dynamic constraints and control constraints ;In the case of unknown target maneuvering strategy, the tracking spacecraft can improve the accuracy of target behavior prediction and the effect of target tracking by iteratively solving the optimal trajectory of the target and the corresponding maneuvering strategy. Because the model predictive control framework is adopted, the present invention can consider control constraints, and has strong robustness, and because the maximum and minimum optimization problems are transformed into multiple quadratic programming problems, the solution is simplified.

Description

technical field [0001] The invention relates to a method for approaching a space non-cooperative target orbit, in particular to a tracking spacecraft orbit control method based on a chase and escape game. Background technique [0002] In the process of recovering non-cooperative space targets, orbital approach operations are required. At present, the control research for this process only considers the estimable state of the target's free drift according to the orbit, for example: [0003] The document "Jagat A, Sinclair A J.Nonlinear Control for Spacecraft Pursuit-Evasion Game Using the State-Dependent Riccati Equation Method[J].IEEETransactions on Aerospace and Electronic Systems,2017,53(6):3032-3042." discloses A spacecraft chase-and-flight game method combined with state-dependent Riccati equations. The method expresses the nonlinear model as a state-dependent linear form, and combines the related theory of linear quadratic differential game to obtain the control strate...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G1/24G05B13/04
CPCB64G1/24G05B13/042
Inventor 罗建军柴源王明明郑子轩马卫华韩楠
Owner RES & DEV INST OF NORTHWESTERN POLYTECHNICAL UNIV IN SHENZHEN