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 in | IEEE transactions on control systems technology Vol. 5; no. 2; pp. 217 - 229 | 
|---|---|
| Main Authors | , | 
| Format | Journal Article | 
| Language | English | 
| Published | 
        New York, NY
          IEEE
    
        01.03.1997
     Institute of Electrical and Electronics Engineers  | 
| Subjects | |
| Online Access | Get full text | 
| ISSN | 1063-6536 | 
| DOI | 10.1109/87.556026 | 
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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. | 
    
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| 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.  | 
    
| Author_xml | – sequence: 1 givenname: M. surname: Bodson fullname: Bodson, M. organization: Dept. of Electr. Eng., Utah Univ., Salt Lake City, UT, USA – sequence: 2 givenname: J.E. surname: Groszkiewicz fullname: Groszkiewicz, J.E.  | 
    
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| Cites_doi | 10.23919/ACC.1988.4790095 10.1109/CDC.1993.325602 10.1109/ACC.1995.533785 10.2514/3.21263 10.1109/MCS.1985.1104940 10.1109/ACC.1995.533784 10.2514/3.20550 10.2514/3.20568 10.1109/7.464346 10.1016/0005-1098(95)98489-S 10.2514/3.21499 10.1109/NAECON.1990.112818 10.1109/ICCON.1989.770576 10.1109/CDC.1993.325275 10.2514/3.21417 10.1109/NAECON.1988.195055 10.1109/7.81428 10.1016/B978-0-12-012724-5.50008-3 10.23919/ACC.1988.4790093 10.2514/3.20412  | 
    
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| Keywords | Least squares method Non linear model Control system Flight Adaptive control Multivariable system Fault tolerant system Reconfiguration  | 
    
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| References_xml | – start-page: 2232 year: 1988 ident: ref13 article-title: application of supercontroller to fighter aircraft reconfiguration publication-title: 1988 American Control Conference ACC doi: 10.23919/ACC.1988.4790095 – ident: ref7 doi: 10.1109/CDC.1993.325602 – ident: ref29 doi: 10.1109/ACC.1995.533785 – year: 1989 ident: ref22 publication-title: Stable Adaptive Systems – ident: ref4 doi: 10.2514/3.21263 – start-page: 586 year: 1984 ident: ref5 article-title: self-repairing flight control system reliability and maintainability program executive overview publication-title: Proc Nat Aerospace Electron Conf – year: 1979 ident: ref16 publication-title: Adaptive Control The Model Reference Approach – ident: ref17 doi: 10.1109/MCS.1985.1104940 – ident: ref3 doi: 10.1109/ACC.1995.533784 – year: 1987 ident: ref30 publication-title: Integrated restructurable flight control system demonstration results – ident: ref15 doi: 10.2514/3.20550 – ident: ref21 doi: 10.2514/3.20568 – year: 1996 ident: ref14 article-title: design guidelines for application of multivariable control theory to aircraft control laws publication-title: Multivariable Control Design Guidelines – ident: ref19 doi: 10.1109/7.464346 – volume: 31 start-page: 597 year: 1995 ident: ref11 article-title: multivariable model reference adaptive control without constraints on the high-frequency gain matrix publication-title: Automatica doi: 10.1016/0005-1098(95)98489-S – year: 1990 ident: ref28 article-title: flight demonstration of the self-repairing flight control system in a nasa f-15 aircraft publication-title: the IEEE National Aerospace and Electronics Conference – ident: ref9 doi: 10.2514/3.21499 – ident: ref1 doi: 10.1109/NAECON.1990.112818 – ident: ref6 doi: 10.1109/ICCON.1989.770576 – start-page: 2242 year: 1993 ident: ref2 article-title: identification with modeling uncertainty and reconfigurable control publication-title: Proc IEEE Conf Decision Contr ” doi: 10.1109/CDC.1993.325275 – start-page: 80 year: 1991 ident: ref27 article-title: nsf workshop on aerospace applications of neurocontrol publication-title: IEEE Contr Syst Mag – year: 1989 ident: ref24 publication-title: Adaptive Control Stability Convergence Robustness – start-page: 400 year: 1986 ident: ref31 article-title: investigation of an automatic trim algorithm for restructurable aircraft control publication-title: Proc Nat Aerospace Electron Conf – ident: ref8 doi: 10.2514/3.21417 – start-page: 906 year: 1985 ident: ref23 article-title: techniques for accommodating control effector failures on a mildly statically unstable airplane publication-title: 1985 American Control Conference ACC – ident: ref12 doi: 10.1109/NAECON.1988.195055 – ident: ref18 doi: 10.1109/7.81428 – year: 1986 ident: ref26 article-title: direct model reference adaptive control for a class of mimo systems publication-title: Control and Dynamic Systems doi: 10.1016/B978-0-12-012724-5.50008-3 – start-page: 616 year: 1987 ident: ref25 article-title: qft digital flight control design as applied to the afti/f-16 publication-title: Proc Nat Aerospace Electron Conf – start-page: 2219 year: 1988 ident: ref10 article-title: a hyperstable model-following flight control system used for reconfiguration following aircraft impairment publication-title: 1988 American Control Conference ACC doi: 10.23919/ACC.1988.4790093 – ident: ref20 doi: 10.2514/3.20412  | 
    
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| 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 | 
    
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