Sliding mode attitude controller design for hypersonic aircraft based on dynamic inverse method and control parameters self-tuning-Reference-Cited by-同舟云学术

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Sliding mode attitude controller design for hypersonic aircraft based on dynamic inverse method and control parameters self-tuning

Published:2023-06-16 Issue: Volume: Page:
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Container-title:Sixth International Conference on Intelligent Computing, Communication, and Devices (ICCD 2023)
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Author:

Cheng Zhihao,Wang Peng

Publisher

SPIE

Reference11 articles.

1. Nonlinear inversion flight control for a supermaneuverable aircraft

2. Reentry Flight Controller Design Using Nonlinear Dynamic Inversion

3. Research and development on theory and algorithms of sliding mode control[J];LIU;Control Theory Applications,2007

4. Sliding mode based trajectory linearization control for hypersonic reentry vehicle via extended disturbance observer

5. Parametric Command Method in Sliding Mode Control for Near Space Vehicle[J];WANG;Journal of Ballistics,2012

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