NDLI: Optimal tracking control of nonlinear dynamic systems with control bounds

Content Provider	IEEE Xplore Digital Library
Author	Lyshevski, S.E.
Copyright Year	1999
Description	Author affiliation: Dept. of Electr. Eng., Purdue Univ., West Lafayette, IN, USA (Lyshevski, S.E.)
Abstract	Using the Hamilton-Jacobi theory, we solve the constrained optimization problem for nonlinear multivariable continuous-time systems. It is illustrated that through the use of positive-definite performance integrands, the designer can analytically synthesize the constrained control laws within the admissible control set. We extend the class of dynamic systems for which the constrained optimization problem can be solved. The paper demonstrates the ability of the constrained optimization concept to design the bounded controller for multivariable advanced aircraft. The fighter longitudinal and lateral dynamics are mapped by a set of nine highly nonlinear differential equations with six bounded control inputs. The complete aircraft model, as derived using the Lagrange equations and nonlinear fluid dynamics, is applied to synthesize an optimal controller using the mechanical limits imposed on the angular deflections of the control surfaces. This very complex multivariable flight control problem for highly nonlinear aircraft have challenged the control community for many years. The results documented in the paper show that a constrained controller synthesized allows one to attain the desired flying and handling qualities and expand the operating envelope. The desired agility, controllability, maneuverability and other pilotage requirements are assessed minimizing the nonquadratic performance cost, and highly detailed nonlinear simulations were performed to demonstrate the advantages of the controller designed.
Starting Page	4810
Ending Page	4815
File Size	458390
Page Count	6
File Format	PDF
ISBN	0780352505
ISSN	01912216
DOI	10.1109/CDC.1999.833304
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	1999-12-07
Publisher Place	USA
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Optimal control Nonlinear control systems Control systems Aerospace control Constraint optimization Aircraft Fluid dynamics Constraint theory Performance analysis Control system synthesis
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

Aircraft flight control system design under state and control bounds

Optimization of nonlinear time-varying systems

Nonlinear receding horizon control of F-16 aircraft

Inverse optimization for a nonlinear system with an input constraint

On the theory of nonlinear systems tracking with guaranteed performance index bounds: application to robot control

Constrained Stochastic Tournament Selection in Flight Control Problems

Optimal control and tracking with eye movement dynamics with and without the Listing's constraint

Robust Adaptive Control for Nonlinear Systems with Hα Tracking Performance: Dynamic Surface Design Approach

Design of nonlinear optimal control system for aircraft with thrust vector

Optimal tracking control of nonlinear dynamic systems with control bounds

Similar Documents

Aircraft flight control system design under state and control bounds

Optimization of nonlinear time-varying systems

Nonlinear receding horizon control of F-16 aircraft

Inverse optimization for a nonlinear system with an input constraint

On the theory of nonlinear systems tracking with guaranteed performance index bounds: application to robot control

Constrained Stochastic Tournament Selection in Flight Control Problems

Optimal control and tracking with eye movement dynamics with and without the Listing's constraint

Robust Adaptive Control for Nonlinear Systems with Hα Tracking Performance: Dynamic Surface Design Approach

Design of nonlinear optimal control system for aircraft with thrust vector

Optimal tracking control of nonlinear dynamic systems with control bounds