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Towards more resilient flight controlLOMBAERTS, Thomas; SMAILI, Hafid; BREEMAN, Jan et al.Fault tolerant flight control (a benchmark challenge). Lecture notes in control and information sciences. 2010, Vol 399, pp 3-45, issn 0170-8643, isbn 978-3-642-11689-6 3-642-11689-2, 1Vol, 43 p.Book Chapter

Flight control century: Triumphs of the systems approachMCRUER, Duane; GRAHAM, Dunstan.Journal of guidance, control, and dynamics. 2004, Vol 27, Num 2, pp 161-173, issn 0731-5090, 13 p.Article

Synthetic-Waypoint Guidance Algorithm for Following a Desired Flight TrajectoryMEDAGODA, Eran D. B; GIBBENS, Peter W.Journal of guidance, control, and dynamics. 2010, Vol 33, Num 2, pp 601-606, issn 0731-5090, 6 p.Article

Multiparadigm design, validation and verification by simulation in flight control system developmentLIU, Hugh H. T.IEEE International Symposium on computer aided control systems design. 2004, pp 71-76, isbn 0-7803-8636-1, 1Vol, 6 p.Conference Paper

Advances techniques for clearance of flight control lawsFielding, Christopher; Varga, Andras; Bennani, Samir et al.Lecture notes in control and information sciences. 2002, issn 0170-8643, isbn 3-540-44054-2, IX, 469 p, isbn 3-540-44054-2Book

Flight Control Software: Mistakes Made and Lessons Learned : SAFETY-CRITICAL SOFTWAREJEPPU, Yogananda.IEEE software. 2013, Vol 30, Num 3, pp 67-72, issn 0740-7459, 6 p.Article

Constrained Linear Quadratic Tracker for Optimal Flight PerformanceDE ALMEIDA, Fabio A; GUERRA, Eduardo Bento; D'OLIVEIRA, Flavio Araripe et al.Journal of guidance, control, and dynamics. 2012, Vol 35, Num 6, pp 1911-1918, issn 0731-5090, 8 p.Article

Exoatmospheric interception problem solved using output feedback lawANDRIEU, V; LAHANIER, H. P.Systems & control letters. 2006, Vol 55, Num 8, pp 633-639, issn 0167-6911, 7 p.Article

Adaptive nonlinear control system design for helicopter robust command augmentationLEE, S; HA, C; KIM, B. S et al.Aerospace science and technology. 2005, Vol 9, Num 3, pp 241-251, issn 1270-9638, 11 p.Article

Design and implementation of a hardware-in-the-loop simulation system for small-scale UAV helicopters : Hardware-in-the-loop simulationGUOWEI CAI; CHEN, Ben M; LEE, Tong H et al.Mechatronics (Oxford). 2009, Vol 19, Num 7, pp 1057-1066, issn 0957-4158, 10 p.Article

Fuel-Efficient Formation Flight-Control Design Based on Energy ManeuverabilityCHOI, Jongug; KIM, Youdan.Journal of guidance, control, and dynamics. 2008, Vol 31, Num 4, pp 1145-1150, issn 0731-5090, 6 p.Article

Full-envelope robust control of a shrouded-fan unmanned vehicleAVANZINI, Giulio; CINIGLIO, Umberto; DE MATTEIS, Guido et al.Journal of guidance, control, and dynamics. 2006, Vol 29, Num 2, pp 435-443, issn 0731-5090, 9 p.Article

Fault Tolerant Flight Control: A SurveyVERHAEGEN, Michel; KANEV, Stoyan; HALLOUZI, Redouane et al.Fault tolerant flight control (a benchmark challenge). Lecture notes in control and information sciences. 2010, Vol 399, pp 47-89, issn 0170-8643, isbn 978-3-642-11689-6 3-642-11689-2, 1Vol, 43 p.Book Chapter

RECOVER: A Benchmark for Integrated Fault Tolerant Flight Control EvaluationSMAILI, Hafid; BREEMAN, Jan; LOMBAERTS, Thomas et al.Fault tolerant flight control (a benchmark challenge). Lecture notes in control and information sciences. 2010, Vol 399, pp 171-221, issn 0170-8643, isbn 978-3-642-11689-6 3-642-11689-2, 1Vol, 51 p.Book Chapter

A frugal fuzzy logic based approach for autonomous flight control of unmanned aerial vehiclesKURNAZ, Sefer; EROGLU, Emre; KAYNAK, Okyay et al.Lecture notes in computer science. 2005, pp 1155-1163, issn 0302-9743, isbn 3-540-29896-7, 1Vol, 9 p.Conference Paper

Decoupling the flight control system of a supersonic vehicleTSAY, Tain-Sou.Aerospace science and technology. 2007, Vol 11, Num 7-8, pp 553-562, issn 1270-9638, 10 p.Article

Precision flight control for a multi-vehicle quadrotor helicopter testbedHOFFMANN, Gabriel M; HAOMIAO HUANG; WASLANDER, Steven L et al.Control engineering practice. 2011, Vol 19, Num 9, pp 1023-1036, issn 0967-0661, 14 p.Article

Oscillatory failure case detection in the A380 electrical flight control system by analytical redundancyGOUPIL, Philippe.Control engineering practice. 2010, Vol 18, Num 9, pp 1110-1119, issn 0967-0661, 10 p.Article

Nonlinear robustness analysis of flight control laws for highly augmented aircraftMENON, Prathyush P; BATES, Declan G; POSTLETHWAITE, Ian et al.Control engineering practice. 2007, Vol 15, Num 6, pp 655-662, issn 0967-0661, 8 p.Article

LMI-based robust flight control of an aircraft subject to CG variationKIM, Jung-Yub; SUNG KYUNG HONG; PARK, Sungsu et al.International journal of systems science. 2010, Vol 41, Num 5, pp 585-592, issn 0020-7721, 8 p.Article

Guidance Algorithm for Range Maximization and Time-of-Flight Control of a Guided ProjectilePHILLIPS, Craig A.Journal of guidance, control, and dynamics. 2008, Vol 31, Num 5, pp 1447-1455, issn 0731-5090, 9 p.Conference Paper

Sliding-mode control for integrated missile autopilot guidanceSHIMA, Tal; IDAN, Moshe; GOLAN, Oded M et al.Journal of guidance, control, and dynamics. 2006, Vol 29, Num 2, pp 250-260, issn 0731-5090, 11 p.Article

Towards a substantially autonomous aerobot for exploration of titanELFES, Alberto; HALL, Jeffery L; MONTGOMERY, James F et al.IEEE International Conference on Robotics and Automation. 2004, pp 2535-2541, isbn 0-7803-8232-3, 5Vol, 7 p.Conference Paper

Capture set computation of an optimally guided missileRAIVIO, Tuomas.Journal of guidance, control, and dynamics. 2001, Vol 24, Num 6, pp 1167-1175, issn 0731-5090Article

Holographic interferometry applied to real-time dynamic modal analysis of an advanced exotic metal alloy airfoil structureFEIN, H.SPIE proceedings series. 1999, pp 89-96, isbn 0-8194-3171-0Conference Paper

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