Integrated Guidance and Autopilot for Dual Controlled Missiles Using Higher Order Sliding Mode Controllers and Observers-Reference-Cited by-同舟云学术

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Integrated Guidance and Autopilot for Dual Controlled Missiles Using Higher Order Sliding Mode Controllers and Observers

Published:2008-06-15 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation and Control Conference and Exhibit
language:
Short-container-title:

Author:

Tournes Christian¹,Shtessel Yuri²

Affiliation:

1. Davidson Technologies

2. The University of Alabam in Huntsville

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-7433

Reference35 articles.

Cited by 7 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Dual-Disturbance-Attenuation-Based Adaptive Guidance Law Against Maneuvering Targets With Practically Finite Time Convergence;2022 41st Chinese Control Conference (CCC);2022-07-25

2. Design of integrated Guidance and control system in the pitch channel using observer based chattering free sliding mode theory;Journal of Control;2020-05-01

3. Guidance Laws With Input Constraints and Actuator Failures;Asian Journal of Control;2015-08-27

4. Partial Integrated Guidance and Control with Impact Angle Constraints;Journal of Guidance, Control, and Dynamics;2015-05

5. Partial integrated missile guidance and control with state observer;Nonlinear Dynamics;2014-12-04

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