In actual engineering cases, the air-breathing hypersonic vehicles are usually propelled by rockets at the ascent stage. Considering the narrow flight corridor of the vehicles and the scramjet ignition requirement, a steady and precise state transition between the two stages is crucial. In this paper, we combine the conventional project trajectory design idea with an improved particle swarm optimization algorithm to find a feasible solution under the actual constraints. A case study is presented to illustrate the effectiveness of the proposed methodology, which is of valuable reference for further research.


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    Title :

    PSO based Ascent Trajectory Optimization for Air-breathing Hypersonic Vehicle


    Contributors:
    He, Runlin (author) / Li, Jinping (author) / Ma, Qinghua (author)


    Publication date :

    2018-08-01


    Size :

    102884 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




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