Trajectory Control of Midcourse Guidance for Air-to-Air Missile Based on Feedback Linearization and Sliding Mode Control

To guarantee the accuracy and energy efficiency of long-distance midcourse guidance for air-to-air missile, a robust trajectory control method based on feedback linearization and sliding mode control is proposed. In guidance loop, the framework of offline trajectory optimization and online tracking...

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Vydané v:	Proceedings of ... IEEE International Conference on Unmanned Systems (Online) s. 1887 - 1892
Hlavní autori:	Zhang, Chencheng, Tong, Zhiqiang, Liu, Hongquan, Pang, Weijian
Médium:	Konferenčný príspevok..
Jazyk:	English
Vydavateľské údaje:	IEEE 18.10.2024
Predmet:	air-to-air missile Atmospheric modeling Feedback linearization midcourse guidance Missiles Nonlinear dynamical systems Perturbation methods Robustness Sliding mode control Tracking loops trajectory control Trajectory optimization Trajectory planning
ISSN:	2771-7372
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