Approximate Solutions of the Optimal AeroassistedCoplanar Transfer of Space Vehicle

Nan Ying; Xiao Yelun; Chen Shilu

Volume 24 Issue 1

Jan. 1998

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Journal of Beijing University of Aeronautics and Astronautics > 1998 > 24(1): 120-123.

Liu Xin, Han Shengqian, Xu Zhikun, et al. Energy-efficient uplink training for downlink multi-antenna transmission[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, (6): 841-846. (in Chinese)

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Nan Ying, Xiao Yelun, Chen Shiluet al. Approximate Solutions of the Optimal AeroassistedCoplanar Transfer of Space Vehicle[J]. Journal of Beijing University of Aeronautics and Astronautics, 1998, 24(1): 120-123. (in Chinese)

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Approximate Solutions of the Optimal AeroassistedCoplanar Transfer of Space Vehicle

1.
Beijung University of Aeronautics and Astronautics,School of Astronautics
2. Northwestern Polytechnical University

Received Date: 09 Jul 1997
Publish Date: 31 Jan 1998

Abstract

Abstract

Green's theorem is employed to find the quantity relationship among the constraints of heating rate,dynamic pressure and lift in reentry flight.The paper deduced the approximate solution of the optimal aeroassisted coplanar trajectories under the three typical constraints.The performance index to be minimized are either heat input,the total dynamic pressure,time during the atmospheric flight,the time integral of the square of the path inclination;or maximize the time of flight during the atmospheric portion of the trajetory.An important conclusion is firstly obtained:under the three constraints above,the optimal aeroassisted coplanar transfers with the first forth kinds payoffs have the same optimal control laws.
- spacecraft,
- orbital mechanics,
- optimization,
- coplanar orbital transfer,
- approximate solution

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References

1. 南英,陈士橹,吕学富,等.航天器再入轨迹与控制进展.导弹与航天运载技术,1994(5):1~10 2. 南英,陈士橹,吕学富.航天器最优再入轨迹的近似解.航天返回与摇感,1994(2):1~10 3. 南英,陈士橹.受多种约束时航天器再入走廊的计算分析.飞行力学,1995(13):18~25 4. Beiner L.Optimal reentry maneuvers with bounded lift control.J of Guidance,1987(10):321~329

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Approximate Solutions of the Optimal AeroassistedCoplanar Transfer of Space Vehicle

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