再入飞行器制导与总体参数的一体化设计

doi:10.3969/j.issn.1674-1579.2014.02.003

Abstract

Abstract: The design of the guidance system for a hypersonic reentry vehicle is presented. The major contributors are discussed, such as aero characteristic, attitude control ability, thermal protective, servo ability, mass, and structure strength. The guidance requirement is needed for early conceptual design. A new approach for guidance overall design is presented. To be appropriate to the vehicle configuration, the guidance law is designed to coordinate the tightly coupled parameters of the vehicle and subsystems.

Key words: hypersonic, reentry vehicle, guidance overall design, system parameters design

CLC Number:

JI Deng-Gao, WU Bin, GUO Zhen-Xi, HUANG Xing-Li. Overall Design of the Guidance and System Parameters for Reentry Vehicle [J]., 2014, 40(2): 14-19.

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URL: http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/10.3969/j.issn.1674-1579.2014.02.003

http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/Y2014/V40/I2/14

References

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Overall Design of the Guidance and System Parameters for Reentry Vehicle

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