Aiming at the Common Aero Vehicle (CAV) entry guidance problem under various trajectory constraints and terminal conditions, an on-board reference trajectory generation method was proposed, and then linear quadratic regulator (LQR) was designed to track the longitudinal reference trajectory. Lateral guidance was realized by using bank-reversal strategy with the aid of the azimuth error corridor. Finally, the entry trajectory was presented based on the above method.


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    Title :

    Entry guidance for Common Aero Vehicle


    Contributors:
    Zhou Wenya, (author) / Chen Hongbo, (author) / Yang Di, (author)


    Publication date :

    2008-12-01


    Size :

    537624 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English





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