NDLI: Mixed H2/H∞ robust adaptive control of hypersonic vehicles based on the characteristic model

Content Provider	IEEE Xplore Digital Library
Author	Huang Huang Yong Wang
Copyright Year	2012
Description	Author affiliation: Beijing Institute of Control Engineering, Beijing 100190, China (Huang Huang; Yong Wang)
Abstract	This paper is concerned with the mixed H2 and H∞ adaptive control of hypersonic vehicles longitudinal dynamics during reentry phase. The dynamics of the angle of attack in the longitudinal plane is modeled by a second-order difference equation known as the characteristic model. In order to improve the transient performance in the presence of large aerodynamic coefficients change and unknown exogenous disturbances, a more intelligent golden-section adaptive control law is proposed based on our previous work. In addition to the easy implementation and stability before the convergence of parameter estimation, this new adaptive control law contains an adjustable parameter λ(k) that guarantees H2 and H∞ robustness of the system, and is calculated based on the linear matrix inequality approach. The integration of adaptive control and robust control provides the attitude system of the hypersonic vehicle with the capability to accommodate large flight conditions in a reliable way. Experiments are carried out on a hypersonic vehicle with a high lift-drag ratio during the reentry phase, and the effectiveness of the control scheme is verified.
Starting Page	2883
Ending Page	2888
File Size	220056
Page Count	6
File Format	PDF
ISBN	9781467325813
ISSN	21612927
e-ISBN	9789881563811
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2012-07-25
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	Chinese Assoc of Automati
Subject Keyword	Adaptation models Characteristic Model Hypersonic Cruise Vehicles Angle of Attack Robust Adaptive Control Aerodynamics Robustness Adaptive control Vehicle dynamics Transient analysis Vehicles
Content Type	Text
Resource Type	Article

Sl.	Authority	Responsibilities	Communication Details
1	Ministry of Education (GoI), Department of Higher Education	Sanctioning Authority	https://www.education.gov.in/ict-initiatives
2	Indian Institute of Technology Kharagpur	Host Institute of the Project: The host institute of the project is responsible for providing infrastructure support and hosting the project	https://www.iitkgp.ac.in
3	National Digital Library of India Office, Indian Institute of Technology Kharagpur	The administrative and infrastructural headquarters of the project	Dr. B. Sutradhar bsutra@ndl.gov.in
4	Project PI / Joint PI	Principal Investigator and Joint Principal Investigators of the project	Dr. B. Sutradhar bsutra@ndl.gov.in Prof. Saswat Chakrabarti will be added soon
5	Website/Portal (Helpdesk)	Queries regarding NDLI and its services	support@ndl.gov.in
6	Contents and Copyright Issues	Queries related to content curation and copyright issues	content@ndl.gov.in
7	National Digital Library of India Club (NDLI Club)	Queries related to NDLI Club formation, support, user awareness program, seminar/symposium, collaboration, social media, promotion, and outreach	clubsupport@ndl.gov.in
8	Digital Preservation Centre (DPC)	Assistance with digitizing and archiving copyright-free printed books	dpc@ndl.gov.in
9	IDR Setup or Support	Queries related to establishment and support of Institutional Digital Repository (IDR) and IDR workshops	idr@ndl.gov.in

Robust adaptive tracking control for air-breathing hypersonic vehicles

Robust adaptive control based on wavelet neural network for a hypersonic vehicle

Adaptive robust control based on T-S fuzzy-neural systems for a hypersonic vehicle

Adaptive mode suppression for aeroelastic hypersonic vehicle

Adaptive exponential time-varying sliding mode control for hypersonic cruise vehicles

Hypersonic vehicle aeroelasticity modeling and analysis based on the induced angle of attack

Characteristic model-based H $_{2}$/H $_{∞}$ robust adaptive control during the re-entry of hypersonic cruise vehicles

Research progresses on characteristic model-based control of hypersonic flight vehicles

Robust and anti-windup control of air-breathing hypersonic cruise vehicle

Mixed H2/H∞ robust adaptive control of hypersonic vehicles based on the characteristic model

Similar Documents

Robust adaptive tracking control for air-breathing hypersonic vehicles

Robust adaptive control based on wavelet neural network for a hypersonic vehicle

Adaptive robust control based on T-S fuzzy-neural systems for a hypersonic vehicle

Adaptive mode suppression for aeroelastic hypersonic vehicle

Adaptive exponential time-varying sliding mode control for hypersonic cruise vehicles

Hypersonic vehicle aeroelasticity modeling and analysis based on the induced angle of attack

Characteristic model-based H $_{2}$/H $_{∞}$ robust adaptive control during the re-entry of hypersonic cruise vehicles

Research progresses on characteristic model-based control of hypersonic flight vehicles

Robust and anti-windup control of air-breathing hypersonic cruise vehicle

Mixed H2/H∞ robust adaptive control of hypersonic vehicles based on the characteristic model