Adaptive Guidance and Control for Autonomous Hypersonic Vehicles

2006 ◽  
Vol 29 (3) ◽  
pp. 725-737 ◽  
Author(s):  
Eric N. Johnson ◽  
Anthony J. Calise ◽  
Michael D. Curry ◽  
Kenneth D. Mease ◽  
J. Eric Corban
Keyword(s):  
Hypersonic Vehicles ◽  
Guidance And Control ◽  
Adaptive Guidance ◽  
And Control

Low-order diving integrated guidance and control for hypersonic vehicles

2019 ◽  
Vol 91 ◽  
pp. 96-109 ◽  
Author(s):  
JianHua Wang ◽  
Long Cheng ◽  
YuanWen Cai ◽  
GuoJian Tang
Keyword(s):  
Hypersonic Vehicles ◽  
Guidance And Control ◽  
Integrated Guidance And Control ◽  
And Control ◽  
Low Order

scholarly journals A Low-Order Partial Integrated Guidance and Control Scheme for Diving Hypersonic Vehicles to Impact Ground Maneuver Target

2021 ◽  
Vol 2021 ◽  
pp. 1-12
Author(s):  
Tong An ◽  
JianHua Wang ◽  
YuLong Pan ◽  
HaiShan Chen
Keyword(s):  
Analytical Model ◽  
Sliding Mode ◽  
Design Method ◽  
Hypersonic Vehicle ◽  
Hypersonic Vehicles ◽  
Dynamic Surface ◽  
Guidance And Control ◽  
Integrated Guidance And Control ◽  
And Control ◽  
Low Order

In this article, a low-order partial integrated guidance and control (PIGC) design method is proposed for diving hypersonic vehicles to impact ground maneuver target. A three-channel analytical model of body rates is deduced based on acceleration components of the hypersonic vehicle. By combining the analytical model of body rates and relative dynamic model between the hypersonic vehicle and target, three-channel commands of body rates are directly generated based on the extended state observer (ESO) technique, sliding mode control approach, and dynamic surface control theory in the guidance subsystem. In the attitude control subsystem, a sliding mode controller is designed to track the commands of body rates and generate commands of control surface fin deflections. By making full use of acceleration information of the hypersonic vehicle measured by the mounted accelerometer, the proposed PIGC design method provides a novel solution to compensate the unknown acceleration of the ground maneuver target. Besides, the order of design model is also reduced, and the design process is simplified. The effectiveness and robustness of the PIGC design method are verified and discussed by 6DOF simulation studies.

Decentralized Mode-Adaptive Guidance and Control for DC Microgrid

2017 ◽  
Vol 32 (1) ◽  
pp. 263-271 ◽  
Author(s):  
Michael D. Cook ◽  
Gordon G. Parker ◽  
Rush D. Robinett ◽  
Wayne W. Weaver
Keyword(s):  
Dc Microgrid ◽  
Guidance And Control ◽  
Adaptive Guidance ◽  
And Control

scholarly journals Integrated adaptive guidance and control of constrained nonlinear air-breathing hypersonic vehicle models

2009 ◽  
Author(s):  
Andrea Serrani ◽  
Alicia M. Zinnecker ◽  
Lisa Fiorentini ◽  
Michael A. Bolender ◽  
David B. Doman
Keyword(s):  
Hypersonic Vehicle ◽  
Air Breathing ◽  
Guidance And Control ◽  
Adaptive Guidance ◽  
And Control
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