Optimality Conditions Applied to Free-Time Multiburn Optimal Orbital Transfers-Reference-Cited by-同舟云学术

Optimality Conditions Applied to Free-Time Multiburn Optimal Orbital Transfers

Published:2016-11 Issue:11 Volume:39 Page:2512-2521
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Chen Zheng¹

Affiliation:

1. University Paris-Saclay, 91405 Orsay, France

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.G000284

Reference32 articles.

1. PontryaginL. S.BoltyanskiV. G.GamkrelidzeR. V.MishchenkoE. F., The Mathematical Theory of Optimal Processes, Interscience, London, 1962, pp. 6–69.

2. Guidance theory and extremal fields

3. Optimality and guidance for planar multiple-burn orbit transfers

4. ChuangC.H.GoodsonT. D.LedsingerL. A. “Multiple Burn Fuel-Optimal Orbital Transfers: Numerical Trajectory Computation and Neighboring Optimal Feedback Guidance,” NASA CR-197317, July 1994–Jan. 1995.

5. Optimal trajectory, guidance, and conjugate points

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