Multi-Process Integrated Planning and Guidance for Return of Reusable Aircraft Under Time Constraint

As the launch frequency of reusable launch vehicle (RLV) increases, the requirement of landing site management is increasing. Especially, the return flight time of RLV should be constrained to improve the utilization of landing site. In this paper, a multi-process integrated (MPI) planning and guida...

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Veröffentlicht in:	IEEE access Jg. 8; S. 179823 - 179836
Hauptverfasser:	Wei, Chang-Zhu, Zhang, Ze, Li, Yuan, Li, Yongyuan
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	Piscataway IEEE 2020 The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Schlagworte:	Acceleration Aerodynamics Aircraft guidance Algorithms backward calculation Computational geometry Computer simulation Constraints convex optimization Convexity Earth Error correction Flight time improved predictor-corrector guidance Interpolation Landing Mathematical analysis Mission planning Monte Carlo simulation Optimization Particle swarm optimization Planning Prediction algorithms Predictor-corrector methods range estimation Reusable launch vehicles RLV time constraint Time factors Trajectory Trajectory optimization Trigonometric functions
ISSN:	2169-3536, 2169-3536
Online-Zugang:	Volltext
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