The path constraints play determinative roles in the entry guidance, hence an aerodynamic model of Common Aero Vehicle (CAV) is established by means of CFD to facilitate the guidance. In the case that the attack angle profile is determined, the bank angle is the only parameter which can be used to control the trajectory in guidance. If the quasi-equilibrium glide condition (QEGC) is used, an entry flight corridor can be obtained by analyzing the path constraints in the entry guidance, and the corridor is transformed into the constraints of the bank angle for the convenience of designing the bank angle profile. Furthermore, a strong robust baseline predictor-corrector algorithm is presented to calculate the value of the bank angle in time. Simulations are provided to verify the effectiveness of the proposed method.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Constrained predictor corrector entry guidance for common aero vehicle


    Contributors:
    Haoliang, Wang (author) / Yongzhao, Hua (author) / Qingdong, Li (author) / Zhang, Ren (author) / Xiwang, Dong (author) / Liang, Han (author) / Peng, Yang (author)


    Publication date :

    2015-07-01


    Size :

    550627 byte





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Constrained Predictor-Corrector Entry Guidance

    Xue, Songbai / Lu, Ping | AIAA | 2010


    Constrained Predictor-Corrector Entry Guidance

    Lu, P. / Xue, S. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2009


    Constrained Predictor-Corrector Entry Guidance

    Lu, Ping / Xue, Songbai | AIAA | 2009


    Predictor-corrector guidance for entry vehicle based on fuzzy logic

    Wang, Tao / Zhang, Hongbo / Tang, Guojian | SAGE Publications | 2019


    Entry guidance for Common Aero Vehicle

    Zhou Wenya, / Chen Hongbo, / Yang Di, | IEEE | 2008