Convex Formulation and Efficiency Enhancement for Powered Landing Guidance With Second-Order Cone Probability Constraints

Real-time trajectory optimization is crucial for achieving autonomous guidance in powered landing. However, the existing algorithms often struggle with uncertainties and are unable to handle second-order cone probability constraints, such as control magnitude and direction constraints. In addition,...

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Veröffentlicht in:	IEEE transactions on aerospace and electronic systems Jg. 61; H. 2; S. 1742 - 1763
Hauptverfasser:	Li, Wenbo, Gong, Shengping
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	New York IEEE 01.04.2025 The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Schlagworte:	Aerospace and electronic systems Algorithms Approximation Constraints Heuristic algorithms Landing simulation Optimal control Optimization Real time Real-time systems Simulation Stochastic processes Trajectory optimization Uncertainty
ISSN:	0018-9251, 1557-9603
Online-Zugang:	Volltext
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