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Volumn 59, Issue 1, 1994, Pages 71-91

Dynamic inversion: An evolving methodology for flight control design

Author keywords

[No Author keywords available]

Indexed keywords


EID: 0003096706     PISSN: 00207179     EISSN: 13665820     Source Type: Journal    
DOI: 10.1080/00207179408923070     Document Type: Article
Times cited : (368)

References (24)
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    • ELGERSMA, M. R., 1986, Nonlinear control, with application to high angle of attack and VSTOL flight. Plan B Project, M.S. thesis, Department of Electrical Engineering, University of Minnesota; 1988, Control of nonlinear systems using partial dynamic inversion. Ph.D. dissertation, University of Minnesota.
    • (1986)
    • Elgersma, M.R.1
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    • Kravaris, C.1
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  • 15
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    • Application of nonlinear transformations to automatic flight control
    • MILITARY SPECIFICATIONS-FLYING QUALITIES OF PILOTED VEHICLES, 1987, MIL-STD-1797A, March
    • MEYER, G., Su, R., and HUNT, L. R., 1984, Application of nonlinear transformations to automatic flight control. Automatica, 1(20). MILITARY SPECIFICATIONS-FLYING QUALITIES OF PILOTED VEHICLES, 1987, MIL-STD-1797A, March.
    • (1984) Automatica , vol.1 , Issue.20
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    • (1987)
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    • Stability of nonlinear inversion control laws applied to nonlinear aircraft pitch-axis models. AFOSR Final Report, Honeywell, October
    • MORTON, B. G., and ENNS, D., 1991, Stability of nonlinear inversion control laws applied to nonlinear aircraft pitch-axis models. AFOSR Final Report, Honeywell, October.
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    • Morton, B.G.1    Enns, D.2
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.