During the time that a hypersonic vehicle experiences the reentry segment, the environment changes dramatically. This paper analyzes all kinds of constraint conditions of the reentry process, then designs the reentry corridor in both the D-V plane and the H-V plane, and analyzes the influence of various factors on the reentry corridor according to that. Based on the constraint conditions, the reentry segment is divided into the initial descent phase, angle of attack recovery phase, overload hold phase and angle of attack transition phase. Meanwhile the rationality of the design is verified by simulation.
Research of Reentry Corridor and Guidance Technology for Hypersonic Vehicle
Advanced Materials Research ; 823 ; 62-66
2013-10-25
5 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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