403
Views
41
CrossRef citations to date
0
Altmetric
Original Articles

1 adaptive controller for tailless unstable aircraft in the presence of unknown actuator failures

, , , &
Pages 705-720 | Received 18 Feb 2008, Accepted 22 May 2008, Published online: 18 Mar 2009

References

  • Brinker , J and Wise , KA . 2000 . “ Flight Testing of a Reconfigurable Flight Control Law on the X-36 Tailless Fighter Aircraft ” . In in Proceedings of the AIAA GNC Conference , Denver : CO .
  • Cao , C and Hovakimyan , N . 2006a . “ Design and Analysis of a Novel ℒ1 Adaptive Control Architecture, Part I: Control Signal and Asymptotic Stability ” . In Proceedings of American Control Conference 3397 – 3402 . Minneapolis, MN
  • Cao , C and Hovakimyan , N . 2006b . “ Design and Analysis of a Novel ℒ1 Adaptive Control Architecture, Part II: Guaranteed Transient Performance ” . In Proceedings of American Control Conference 3403 – 3408 . Minneapolis, MN
  • Cao , C and Hovakimyan , N . 2006c . “ Novel ℒ1 Neural Network Adaptive Control Architecture with Guaranteed Transient Performance ” . In IEEE Transactions on Neural Networks 18, 1160–1171
  • Cao , C and Hovakimyan , N . 2007a . “ Guaranteed Transient Performance with ℒ1 Adaptive Controller for Systems with Unknown Time-varying Parameters and Bounded Disturbances ” . In American Control Conference 3925 – 3930 . New York City, NY
  • Cao , C and Hovakimyan , N . 2007b . “ Stability Margins of ℒ1 Adaptive Control Architecture ” . In in American Control Conference 3931 – 3936 . New York City, NY
  • Cao , C , Patel , VV , Reddy , CK , Hovakimyan , N , Lavretsky , E and Wise. , K . 2006 . “ Are Phase and Time-delay Margins Always Adversely Affected by High-Gain? ” . In AIAA Guidance, Navigation, and Control Conference AIAA Paper No. 2006-6347
  • Corban , J , Burkemper , V , Holt , K , Evers , J , Calise , A and Sharma , M . 2002 . “ Flight Test of an Adaptive Autopilot for Precision Guided Munitions ” . In Proceedings of the AIAA Missile Sciences Conference 5 – 7 . Monterey, CA
  • Kim , BS and Calise , AJ . 1997 . Nonlinear Flight Control Using Neural Networks . Journal of Guidance, Control and Dynamics , 52 : 26 – 33 .
  • Lavretsky , E and Hovakimyan , N . 2004 . “ Positive-Modification for Stable Adaptation in a Class of Nonlinear Systems with Actuator Constraints ” . In Proceedings of American Control Conference 2545 – 2550 . Boston, MA
  • Lavretsky , E and Wise , K . 2005 . “ Adaptive Flight Control for Manned/Unmanned Military Aircraft ” . In Proceedings of American Control Conference , Portland : OR .
  • McFarland , M and Calise , A . 1996 . “ Neural-adaptive Nonlinear Autopilot Design for an Agile Anti-air Missile ” . In in Proceedings of the AIAA GNC Conference San Diego, CA Paper AIAA 96-3914
  • McFarland , M and Calise , A . 1997 . “ Multi-layer Neural Networks and Adaptive Non-linear Control of for Agile Anti-air Missiles ” . In Proceedings of the AIAA GNC Conference , New Orleans : LA . Paper AIAA 97-3540
  • Patel , V , Cao , C , Hovakimyan , N , Wise , K and Lavretsky , E . 2007 . “ ℒ1 Adaptive Controller for Tailless Unstable Aircraft ” . In American Control Conference 5272 – 5277 . New York City, NY
  • Pomet , JB and Praly , L . 1992 . Adaptive Nonlinear Regulation: Estimation from Lyapunov Equation . IEEE Transctions on Automatic Control , 37 : 729 – 740 .
  • Sharma , M and Calise , A . 2001 . “ Neural Network Augmentation of Existing Linear Controllers ” . In Proceedings of the AIAA GNC Conference Montreal, , Canada AIAA Paper No, 2001-4163
  • Sharma , M , Calise , AJ and Corban , JE . 2000 . “ Application of an Adaptive Autopilot Design to a Family of Guided Munitions ” . In Proceedings of the AIAA GNC Conference Denver, CO AIAA Paper No, 2000-3969
  • Sharma , M , Wise , K and Lavretsky , E . 2006 . “ Application and Flight Testing of an Adaptive Autopilot on Precision Guided Munitions ” . In Proceedings Of the 2006 AIAA Guidance, Navigation, and Control Conference Keystone, CO AIAA Paper No. 2005-6568
  • Steinberg , M . 2005 . Historical Overview of Research in Reconfigurable Flight Control . Proceedings of the Institution of Mechanical Engineers. Part G: Journal of Aerospace Engineering , 219 : 263 – 275 .
  • Urnes-Jr , JE . 1999 . “ NASA F-15 Intelligent Flight Control ” . In Final Report , St Louis, MO : Boeing Report No. STL 99P0040 .
  • Ward , DE . 1998 . Self Designing Controller , Final Report, AFRL WL-TR-97-3095
  • Wise , KA . “Reconfigurable Systems for Tailless Fighter Aircraft - RESTORE” . In Final Report, AFRL-VA–WP-TR-99-3067
  • Wise , KA . 1990 . Bank-to-turn Missile Autopilot Design using Loop Transfer Recovery . Journal of Guidance, Control, and Dynamics , 13 : 145 – 152 .
  • Wise , KA and Brinker , JS . 1996 . Linear Quadratic Flight Control for Ejection Seats . Journal of Guidance, Control, and Dynamics , 19 : 15 – 22 .
  • Wise , K and Brinker , J . 1998 . “ Reconfigurable Flight Control for a Tailless Advanced Fighter Aircraft ” . In Proceedings of the AIAA GNC Conference , 75 – 87 . Boston : MA .
  • Wise , K , Brinker , J , Calise , A , Enns , D , Elgersma , M and Voulgaris , P . 1999 . Direct Adaptive Reconfigurable Flight Control for a Tailless Advanced Fighter Aircraft . International Journal of Robust Nonlinear Control, Special Issue on Reconfigurable Flight Control , 9 : 999 – 1012 .
  • Wise , KA and Deylami , F . 1991 . “ Approximating a Linear Quadratic Missile Autopilot Design Using an Output Feedback Projective Control ” . In Proceedings of the AIAA Guidance, Navigation, and Control Conference , 114 – 122 . New Orleans : LA . Paper AIAA 91-2613
  • Wise , KA , Lavretsky , E and Hovakimyan , N . 2006 . “ Adaptive Control of Flight: Theory, Applications, and Open Problems', 2006 ACC ” . In Minneapolis MN, also presented at the Thirteenth Yale Workshop on Adaptive and Learning Systems , Connecticut : New Haven .
  • Wise , K , Lavretsky , E , Zimmerman , J , Francis-Jr , J , Dixon , D and Whitehead , B . 2005 . “ Adaptive Flight Control of a Sensor Guided Munition. ” . In Proceedings of AIAA Guidance, Navigation and Control Conference San Francisco, CA AIAA Paper No. 2005-6385

Reprints and Corporate Permissions

Please note: Selecting permissions does not provide access to the full text of the article, please see our help page How do I view content?

To request a reprint or corporate permissions for this article, please click on the relevant link below:

Academic Permissions

Please note: Selecting permissions does not provide access to the full text of the article, please see our help page How do I view content?

Obtain permissions instantly via Rightslink by clicking on the button below:

If you are unable to obtain permissions via Rightslink, please complete and submit this Permissions form. For more information, please visit our Permissions help page.