We investigate the pursuit–evasion differential game (PE Game) for satellites with continuous thrust from the viewpoint of reachable domain (RD). A concept of hyper-reachable domain (HRD) is introduced to help analyze the problem, and a sufficient condition for capture in a PE Game is proposed based on the players’ HRD. Meanwhile, to practically use the RD as a tool to analyze the PE Game, an analytical form of the satellite's reachable domain is deduced based on the Clohessy Wiltshire (CW) model. The simplicity and accuracy of the CW model in solving the RD render it practicable to apply the sufficient condition in studying the PE Game of continuous-thrust satellites.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Pursuit–Evasion Game for Satellites Based on Continuous Thrust Reachable Domain


    Contributors:


    Publication date :

    2020-12-01


    Size :

    2401814 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



    Spacecraft Rendezvous and Pursuit/Evasion Analysis Using Reachable Sets

    Venigalla, Chandrakanth / Scheeres, Daniel | AIAA | 2018



    Satellite proximate pursuit-evasion game with different thrust configurations

    Ye, Dong / Shi, Mingming / Sun, Zhaowei | BASE | 2020

    Free access


    Spacecraft Rendezvous and Pursuit/Evasion Analysis Using Reachable Sets (AIAA 2018-0219)

    Venigalla, Chandrakanth / Scheeres, Daniel | British Library Conference Proceedings | 2018