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Volumn , Issue , 2001, Pages

Selection of longitudinal desired dynamics for dynamic inversion controlled re-entry vehicles

Author keywords

[No Author keywords available]

Indexed keywords


EID: 84894455746     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (20)

References (24)
  • 4
    • 0003096706 scopus 로고
    • Dynamic Inversion: An Evolving Methodology for Flight Control Design
    • Enns,D.,Bugajski,D.,Hendrick,R.,and Stein,G.,'Dynamic Inversion: An Evolving Methodology for Flight Control Design,'InternationalJournal of Control,Vol. 59,No. 1,1994,pp.71-91.
    • (1994) InternationalJournal of Control , vol.59 , Issue.1 , pp. 71-91
    • Enns, D.1    Bugajski, D.2    Hendrick, R.3    Stein, G.4
  • 6
    • 0027617350 scopus 로고
    • Robust Flight Control Design Using Dynamics Inversion and Structured Singular Value Synthesis
    • June
    • Adams,RJ. and Banda,S.V.,'Robust Flight Control Design Using Dynamics Inversion and Structured Singular Value Synthesis,' IEEE Transactions on Control Systems Technology,Vol. 1,No. 2,June 1993,pp. 80-92.
    • (1993) IEEE Transactions On Control Systems Technology , vol.1 , Issue.2 , pp. 80-92
    • Adams, R.J.1    Banda, S.V.2
  • 9
    • 84959177312 scopus 로고    scopus 로고
    • An Approach to Select Desired Dynamics Gains for Dynamic Inversion Control Laws
    • AIAA Paper 97-3607,New Orleans,LA,Aug
    • Per,H. and Enns,D.F.,'An Approach to Select Desired Dynamics Gains for Dynamic Inversion Control Laws,' AIAA Paper 97-3607,Proceedings of the AIAA Guidance,Navigation,and Control Conference,New Orleans,LA,Aug. 1997. pp. 755-769.
    • (1997) Proceedings of the AIAA Guidance,Navigation,and Control Conference , pp. 755-769
    • Per, H.1    Enns, D.F.2
  • 11
    • 0003093484 scopus 로고
    • Preliminary Assessment of the Robustness of Dynamic Inversion Based Flight Control Laws
    • AIAA Paper 92-4330,Hilton Head Island,SC,Aug
    • Snell,S.A.,'Preliminary Assessment of the Robustness of Dynamic Inversion Based Flight Control Laws,AIAA Paper 92-4330,Proceedings of the AIAA Guidance,Navigation and Control Conference,Hilton Head Island,SC,Aug. 1992,pp.206-216.
    • (1992) Proceedings of the AIAA Guidance,Navigation and Control Conference , pp. 206-216
    • Snell, S.A.1
  • 12
    • 84959170698 scopus 로고    scopus 로고
    • Robust Control of Angle of Attack Using Dynamic Inversion Combined with Quantitative Feedback Theory
    • AIAA Paper 96-3783,Hilton Head Island,SC,July
    • Snell,S.A. and Stout,P.W.,'Robust Control of Angle of Attack Using Dynamic Inversion Combined with Quantitative Feedback Theory,' AIAA Paper 96-3783,Proceedings of the AIAA Guidance,Navigation and Control Conference,Hilton Head Island,SC,July 1996,pp. 1-12.
    • (1996) Proceedings of the AIAA Guidance,Navigation and Control Conference , pp. 1-12
    • Snell, S.A.1    Stout, P.W.2
  • 13
    • 0030290057 scopus 로고    scopus 로고
    • Stability and Flying Qualities Robustness of a Dynamic Inversion Aircraft Control Law
    • Nov.-Dec
    • Drinker,J.S. and Wise,K.A.,'Stability and Flying Qualities Robustness of a Dynamic Inversion Aircraft Control Law,' Journal of Guidance,Control,and Dynamics,Vol. 19,No. 6,Nov.-Dec.,1996,pp.l270-1277.
    • (1996) Journal of Guidance,Control,and Dynamics , vol.19 , Issue.6
    • Drinker, J.S.1    Wise, K.A.2
  • 14
    • 0029210924 scopus 로고
    • Robust Dynamic Inversion for Control of Highly Maneuverable Aircraft
    • Jan.-Feb
    • Reiner,J.,Balas,G.J.,and Garrard,W.L.,'Robust Dynamic Inversion for Control of Highly Maneuverable Aircraft,' Journal of Guidance,Control and Dynamics,Vol. 18,No. 1,Jan.-Feb. 1995,pp. 18-24.
    • (1995) Journal of Guidance,Control and Dynamics , vol.18 , Issue.1 , pp. 18-24
    • Reiner, J.1    Balas, G.J.2    Garrard, W.L.3
  • 16
    • 84894477357 scopus 로고    scopus 로고
    • Application of Multivariable Control Theory to Aircraft Control Laws: Final Report: Multivariable Control Design Guidelines
    • Honeywell Technology Center,Lockheed Martin Skunk Works,and Lockheed Martin Tactical Aircraft Systems,Wright Laboratory,WL-TR-96-3099,Wright-Patterson AFB,OH,May
    • Honeywell Technology Center,Lockheed Martin Skunk Works,and Lockheed Martin Tactical Aircraft Systems,'Application of Multivariable Control Theory to Aircraft Control Laws: Final Report: Multivariable Control Design Guidelines,' Flight Dynamics Directorate,Wright Laboratory,WL-TR-96-3099,Wright-Patterson AFB,OH,May 1996.
    • (1996) Flight Dynamics Directorate
  • 20
    • 84894469813 scopus 로고    scopus 로고
    • Internal Memo,NASA Johnson Space Center,Houston,TX,May
    • Anon.,'X-38 V131R FCS Requirements,' Internal Memo,NASA Johnson Space Center,Houston,TX,May 2000.
    • (2000) X-38 V131R FCS Requirements
    • Anon1
  • 22
    • 0142227122 scopus 로고    scopus 로고
    • Robust Dynamic Inversion Controller Design and Analysis to the X-38 Vehicle
    • AIAA Paper 2001-4380,Montreal,Canada,Aug
    • Ito,D. and Valasek,J.,'Robust Dynamic Inversion Controller Design and Analysis to the X-38 Vehicle,' AIAA Paper 2001-4380,AIAA Guidance,Navigation and Control Conference,Montreal,Canada,Aug. 2001.
    • (2001) AIAA Guidance,Navigation and Control Conference
    • Ito, D.1    Valasek, J.2
  • 23
    • 0019531761 scopus 로고
    • Multivariable Feedback Design: Concepts for a Classical/Modern Synthesis
    • Feb
    • Doyle,J.C. and Stein,G.,'Multivariable Feedback Design: Concepts for a Classical/Modern Synthesis,' IEEE Transactions on Automatic Control,Vol. AC-29,No. 1,Feb. 1981,pp. 4-16.
    • (1981) IEEE Transactions On Automatic Control , vol.29 , Issue.1 AC , pp. 4-16
    • Doyle, J.C.1    Stein, G.2
  • 24
    • 0024689932 scopus 로고
    • Analysis of a Candidate Control Algorithm for a Ride-Quality Augmentation System
    • July-Aug
    • Suikat,R.,Donaldson,K.,and Downing,D.,'Analysis of a Candidate Control Algorithm for a Ride-Quality Augmentation System,' Journal of Guidance,Control and Dynamics,Vol. 12,No. 4,July-Aug. 1989,pp,505-513.
    • (1989) Journal of Guidance,Control and Dynamics , vol.12 , Issue.4 , pp. 505-513
    • Suikat, R.1    Donaldson, K.2    Downing, D.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.