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Volumn 27, Issue 6, 2004, Pages 1017-1027

Nonlinear control allocation using piecewise linear functions

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT; ALGORITHMS; CLOSED LOOP CONTROL SYSTEMS; CONSTRAINT THEORY; DATABASE SYSTEMS; LINEAR CONTROL SYSTEMS; RUDDERS;

EID: 9944238904     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.9546     Document Type: Article
Times cited : (64)

References (18)
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    • Ngo, A.1    Doman, D.2
  • 5
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    • Modular control law design for the innovative control effectors (ICE) tailless fighter aircraft configuration 101-3
    • U.S. Air Force Research Lab., Wright-Patterson AFB, OH, June
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    • (1999) Tech. Rept. , vol.AFRL-VA-WP-TR 1999-3057
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    • Evaluation of optimization methods for control allocation
    • Bodson, M., "Evaluation of Optimization Methods for Control Allocation," Journal of Guidance, Control, and Dynamics, Vol. 25, No. 4, 2002, pp. 703-711.
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    • Bodson, M.1
  • 7
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    • A closed-loop comparison of control allocation methods
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    • Page, A., and Steinberg, M. L., "A Closed-Loop Comparison of Control Allocation Methods," AIAA Paper 00-37180, Aug. 2000.
    • (2000) AIAA Paper 00-37180
    • Page, A.1    Steinberg, M.L.2
  • 8
    • 85087192339 scopus 로고    scopus 로고
    • High-fidelity simulation testing of control allocation methods
    • May
    • Page, A. B., and Steinberg, M. L., "High-Fidelity Simulation Testing of Control Allocation Methods," AIAA Paper 2002-4547, May 2002.
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  • 10
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    • Attainable moments for the constrained control allocation problem
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  • 11
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    • Ikeda, Y., Hood, M., and Boiling, J., "Maximum Attainable Moment Space with LI Optimization," AIAA Paper 01-37198, Aug. 2001.
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  • 12
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    • Improving control allocation accuaracy for nonlinear aircraft dynamics
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  • 14
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  • 18
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.