Research of Reentry Corridor and Guidance Technology for Hypersonic Vehicle

Xin Min Wang; Peng Zhang; Cong Chao Yao

doi:10.4028/www.scientific.net/AMR.823.62

Paper Titles

The Analysis and Design of a New Type Wedge Surfaces of Sprag Overrunning Clutch
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The Linear Optimal Control for the Mechanical Vibration Based on Remanufacturing Repaired
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The NC Grinding Machine Rebuilding for TG30 NC Lathe
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The Application of DSP for Controlling Stepper Motor
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Research of Reentry Corridor and Guidance Technology for Hypersonic Vehicle
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A Dynamic Film Thickness Control System Based on Automatic Wind Ring
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Multifunctional Special Vehicle Design for the Viaduct Maintenance Based on Solidworks
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The Panoramic Vision Simulation System for Loading/Unloading in Container Yard
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Servo Control System of NC Modifying Forming Grinding Wheel Based on Cross Coupling Theory
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HomeAdvanced Materials ResearchAdvanced Materials Research Vol. 823Research of Reentry Corridor and Guidance...

Research of Reentry Corridor and Guidance Technology for Hypersonic Vehicle

Abstract:

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.