Multivariable adaptive algorithms for reconfigurable flight control

The application of multivariable adaptive control techniques to flight control reconfiguration is considered. The objective is to redesign automatically flight control laws to compensate for actuator failures or surface damage. Three adaptive algorithms for multivariable model reference control are...

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Published inIEEE transactions on control systems technology Vol. 5; no. 2; pp. 217 - 229
Main Authors Bodson, M., Groszkiewicz, J.E.
Format Journal Article
LanguageEnglish
Published New York, NY IEEE 01.03.1997
Institute of Electrical and Electronics Engineers
Subjects
Online AccessGet full text
ISSN1063-6536
DOI10.1109/87.556026

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Abstract The application of multivariable adaptive control techniques to flight control reconfiguration is considered. The objective is to redesign automatically flight control laws to compensate for actuator failures or surface damage. Three adaptive algorithms for multivariable model reference control are compared. The availability of state measurements in this application leads to relatively simple algorithms. The respective advantages and disadvantages of the adaptive algorithms are discussed, considering their complexity and the assumptions that they require. An equation-error based algorithm is found to be preferable. Simulations obtained using a full nonlinear model of a twin-engine jet aircraft are presented. The results demonstrate the ability of the adaptive algorithms to maintain trim after a failure, to restore tracking of the pilot commands despite the loss of actuator effectiveness, and to coordinate the use of the remaining active control surfaces in order to guarantee the decoupling of the rotational axes. A new adaptive algorithm with a variable forgetting feature is also used and is found to yield a useful alternative to covariance resetting as a solution to covariance wind-up in least-squares algorithms.
AbstractList The application of multivariable adaptive control techniques to flight control reconfiguration is considered. The objective is to redesign automatically flight control laws to compensate for actuator failures or surface damage. Three adaptive algorithms for multivariable model reference control are compared. The availability of state measurements in this application leads to relatively simple algorithms. The respective advantages and disadvantages of the adaptive algorithms are discussed, considering their complexity and the assumptions that they require. An equation-error based algorithm is found to be preferable. Simulations obtained using a full nonlinear model of a twin-engine jet aircraft are presented. The results demonstrate the ability of the adaptive algorithms to maintain trim after a failure, to restore tracking of the pilot commands despite the loss of actuator effectiveness, and to coordinate the use of the remaining active control surfaces in order to guarantee the decoupling of the rotational axes. A new adaptive algorithm with a variable forgetting feature is also used and is found to yield a useful alternative to covariance resetting as a solution to covariance wind-up in least-squares algorithms
The application of multivariable adaptive control techniques to flight control reconfiguration is considered. The objective is to redesign automatically flight control laws to compensate for actuator failures or surface damage. Three adaptive algorithms for multivariable model reference control are compared. The availability of state measurements in this application leads to relatively simple algorithms. The respective advantages and disadvantages of the adaptive algorithms are discussed, considering their complexity and the assumptions that they require. An equation-error based algorithm is found to be preferable. Simulations obtained using a full nonlinear model of a twin-engine jet aircraft are presented. The results demonstrate the ability of the adaptive algorithms to maintain trim after a failure, to restore tracking of the pilot commands despite the loss of actuator effectiveness, and to coordinate the use of the remaining active control surfaces in order to guarantee the decoupling of the rotational axes. A new adaptive algorithm with a variable forgetting feature is also used and is found to yield a useful alternative to covariance resetting as a solution to covariance wind-up in least-squares algorithms.
Author Groszkiewicz, J.E.
Bodson, M.
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Issue 2
Keywords Least squares method
Non linear model
Control system
Flight
Adaptive control
Multivariable system
Fault tolerant system
Reconfiguration
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Snippet The application of multivariable adaptive control techniques to flight control reconfiguration is considered. The objective is to redesign automatically flight...
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StartPage 217
SubjectTerms Actuators
Adaptative systems
Adaptive algorithm
Adaptive control
Aerodynamics
Aerospace control
Aircraft propulsion
Applied sciences
Automatic control
Computer science; control theory; systems
Control system synthesis
Control theory. Systems
Exact sciences and technology
Fault tolerant systems
Nonlinear dynamical systems
Nonlinear equations
Title Multivariable adaptive algorithms for reconfigurable flight control
URI https://ieeexplore.ieee.org/document/556026
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https://www.proquest.com/docview/28938129
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