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Supervised by Ministry of Industry and Information Technology of The People's Republic of China Sponsored by Harbin Institute of Technology Editor-in-chief Yu Zhou ISSNISSN 1005-9113 CNCN 23-1378/T

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Related citation:ZHOU Wen-ya,YANG Di,CHEN Hong-bo.Maneuver strategy of lifting reentry vehicle[J].Journal of Harbin Institute Of Technology(New Series),2010,17(3):333-337.DOI:10.11916/j.issn.1005-9113.2010.03.008.
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Maneuver strategy of lifting reentry vehicle
Author NameAffiliation
ZHOU Wen-ya Dept of Astronautics,Harbin Institute of Technology,Harbin 150001,China 
YANG Di Dept of Astronautics,Harbin Institute of Technology,Harbin 150001,China 
CHEN Hong-bo China Academy of Launch Vehicle Technology,Beijing 100076,China 
Abstract:
An optimal maneuver strategy is proposed for lifting reentry vehicle to reach the maximum lateral range after reentering the atmosphere. Aiming at problems that too many co-state variables and difficulty in estimating the initial values of co-state variables,the equilibrium glide condition (EGC) is utilized to reduce the reentry motion equations and then the optimal maneuver strategy satisfied above performance index is derived. This maneuvering strategy is applied to the lifting reentry weapon platform CAV which was designed by America recently to realize both longitudinal and lateral trajectory design by controlling the attack angle and the bank angle respectively. The simulation result indicates that the maneuver strategy proposed enables CAV to reach favorable longitudinal range and lateral range.
Key words:  optimal maneuver strategy  lifting reentry vehicle  EGC  trajectory design  Gauss pseudospectral method
DOI：10.11916/j.issn.1005-9113.2010.03.008
Clc Number:V412.44
Fund:

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