Nonlinear Optimal Midcourse Guidance Using Sequential Pseudospectral Model Predictive Control

A sequential pseudospectral model predictive control (SPMPC) method is proposed for nonlinear optimal midcourse guidance with a general performance index. First, the optimal midcourse guidance problem is formulated as a standard Bolza optimal control problem. Then, integral prediction and Taylor exp...

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Veröffentlicht in:	IEEE transactions on aerospace and electronic systems Jg. 61; H. 5; S. 14463 - 14478
Hauptverfasser:	Xu, Xiang, Chen, Wanchun, Yang, Liang
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	New York IEEE 01.10.2025 The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Schlagworte:	Aerodynamics Aerospace and electronic systems Calculus of variations Computational efficiency Exact solutions Mathematical analysis Mathematical models Midcourse guidance Missiles Monte Carlo simulation Optimal control Optimization Performance analysis Performance indices Polynomials Prediction algorithms Predictive control Quadratic equations Taylor series Terminal velocity Trajectory
ISSN:	0018-9251, 1557-9603
Online-Zugang:	Volltext
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