After generating reference trajectory in the process of reentry guidance for reusable launch vehicle, if the designed bank angle curve is too close to the constraint boundary, there is a great possibility for the obtained reference trajectory to exceed the reentry corridor boundary. This paper proposed a margin searching method, to reduce the likelihood of generating a reference trajectory which exceeds the reentry corridor boundary and to improve the design success rate.


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    Title :

    Improved reference trajectory generation method in reentry guidance


    Contributors:
    Xiong, Z. H. (author) / Chen, J. (author) / Yi, K. (author) / Zhao, Q. L. (author) / Li, Q. D. (author) / Ren, Z. (author)


    Publication date :

    2014-08-01


    Size :

    323005 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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