Modelling and Simulation of a Fault-Tolerant Flight Control System
Author:
Affiliation:
1. Department of Mechanical and Aerospace Engineering, West Virginia University, Morgantown, WV 26506/6106,USA; e-mail: {, , }, {,
2. Department of Electrical Systems, University of Perugia, Perugia, Italy;
Publisher
Informa UK Limited
Subject
Electrical and Electronic Engineering,Hardware and Architecture,Mechanics of Materials,Modelling and Simulation,Software
Link
https://www.tandfonline.com/doi/pdf/10.1080/02286203.2006.11442345
Reference8 articles.
1. J. Totah, Adaptive flight control and Online learning,Proc. AIAA Guidance, Navigation and Control Conf., New Orleans, LA, 1997, 373–380
2. J.S. Brinker & K. Wise, Flight testing of a reconfigurable flight control law on the X-36 Tailless Fighter Aircraft,Proc. AIAA Guidance, Navigation, and Controls Conf., New Orleans, LA, 2000, 903–909
3. Intelligent flight control: Advanced concept program — Annual report(St. Louis, Missouri: McDonnell Douglas Aerospace, 1997)
4. E.A. Morelli, Real-time parameter estimation in the frequency domain,Proc. AIAA Atmospheric Flight Mechanics Conf., Portland, OR, 1999, 477–487
5. J. Roskam,Airplane flight dynamics and automatic flight controls: Part I(Ottawa, KA: Roskam Aviation and Engineering Corporation, 1994)
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