A Fault-Tolerant Control Architecture for Unmanned Aerial Vehicles
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[1] B. Saha,et al. A Fault Detection and Reconfigurable Control Architecture for Unmanned Aerial Vehicles , 2005, 2005 IEEE Aerospace Conference.
[2] S. Glavaski,et al. Reconfigurable control for active management of aircraft system failures , 2001, Proceedings of the 2001 American Control Conference. (Cat. No.01CH37148).
[3] John D. Schierman,et al. Reconfigurable control for VTOL UAV shipboard landing , 1999 .
[4] Jian Wang,et al. Reliable Automatic Landing Control against Actuator Stuck Faults , 2004 .
[5] Jin Jiang,et al. A stability guaranteed active fault-tolerant control system against actuator failures , 2001, Proceedings of the 40th IEEE Conference on Decision and Control (Cat. No.01CH37228).
[6] George,et al. Rotary Wing Final Experiments for the Software Enabled Control Program , 2005 .
[7] Jovan D. Boskovic,et al. A multilayer control architecture for unmanned aerial vehicles , 2002, Proceedings of the 2002 American Control Conference (IEEE Cat. No.CH37301).
[8] Anthony J. Calise,et al. Adaptive Output Feedback for Altitude Control of an Unmanned Helicopter Using Rotor RPM , 2004 .
[9] George Vachtsevanos,et al. INTELLIGENT CONTROL OF UNMANNED AERIAL VEHICLES FOR IMPROVED AUTONOMY AND RELIABILITY , 2004 .
[10] Wright-Patterson Afb,et al. Integration of On-line System Identification and Optimization-based Control Allocation* , 1998 .
[11] Sai-Ming Li,et al. On-line failure detection and identification (FDI) and adaptive reconfigurable control (ARC) in aerospace applications , 2001, Proceedings of the 2001 American Control Conference. (Cat. No.01CH37148).
[12] David G. Ward,et al. Development and Flight Testing of a Parameter Identification Algorithm for Reconfigurable Control , 1998 .
[13] Michael A. Bolender,et al. A Method for Estimating Control Failure Effects for Aerodynamic Vehicle Trajectory Retargeting , 2004 .
[14] Eric N. Johnson,et al. Limited authority adaptive flight control , 2000 .
[15] S. R. Wells,et al. Sliding mode control applied to reconfigurable flight control design , 2002 .
[16] Jin Jiang,et al. An interacting multiple-model based fault detection, diagnosis and fault-tolerant control approach , 1999, Proceedings of the 38th IEEE Conference on Decision and Control (Cat. No.99CH36304).
[17] K. Sobel,et al. Eigenstructure assignment for design of multimode flight control systems , 1985, IEEE Control Systems Magazine.
[18] Manuela Battipede,et al. Adaptive Neurocontroller for a Nonlinear Combat Aircraft model , 1998 .
[19] G. Biswas,et al. Diagnostic/prognostic modeling and reconfigurable control , 2004, Proceedings AUTOTESTCON 2004..
[20] Marc Bodson,et al. Evaluation of optimization methods for control allocation , 2001 .
[21] William Wang,et al. Petri Net Based Modeling Approach for Fault Affected UAV Subsystems Reconfiguration , 2004 .
[22] Roberto Celi,et al. Reconfigurable Flight Control Systems for a Tandem Rotor Helicopter , 1996 .
[23] Wright-Patterson Afb,et al. Regularization Techniques for Real-Time Identification of Aircraft Parameters , 1997 .
[24] Stephen Osder,et al. Practical View of Redundancy Management Application and Theory , 1999 .
[25] Jae Weon Choi,et al. An indirect adaptive control using eigenstructure assignment , 2001, SICE 2001. Proceedings of the 40th SICE Annual Conference. International Session Papers (IEEE Cat. No.01TH8603).
[26] Eric N. Johnson,et al. Latency Compensation in an Adaptive Flight Controller , 2003 .
[27] John D. Schierman,et al. Flight Test Results of an Adaptive Guidance System for Reusable Launch Vehicles , 2004 .
[28] Eric Feron,et al. Trajectory reconfiguration for an unmanned aircraft , 2002 .
[29] Eugene A. Morelli,et al. Flight Investigation of Prescribed Simultaneous Independent Surface Excitations for Real-Time Parameter Identification , 2003 .
[30] Rahmat A. Shoureshi,et al. On implementation of active control systems , 1995, Proceedings of 1995 American Control Conference - ACC'95.
[31] A. Page,et al. A CLOSED-LOOP COMPARISON OF CONTROL ALLOCATION METHODS , 2000 .
[32] Marc Bodson. Self-Designing Control Systems for Piloted and Uninhabited Aerial Vehicles , 2001 .
[33] Charles C. Jorgensen,et al. Direct Adaptive Aircraft Control Using Dynamic Cell Structure Neural Networks , 1997 .
[34] Marc Bodson,et al. Multivariable adaptive algorithms for reconfigurable flight control , 1997, IEEE Trans. Control. Syst. Technol..
[35] Youmin Zhang,et al. Design of integrated fault detection, diagnosis and reconfigurable control systems , 1999, Proceedings of the 38th IEEE Conference on Decision and Control (Cat. No.99CH36304).
[36] R. Mehra,et al. Robust Adaptive Variable Structure Control of Spacecraft Under Control Input Saturation , 2001 .
[37] John Hunt,et al. State-Dependent Riccati Equation Control of a Small Unmanned Helicopter , 2003 .
[38] Eric N. Johnson,et al. Application of Software Enabled Control Technologies to a Full-Scale Unmanned Helicopter , 2005 .
[39] Meir Pachter,et al. Reconfigurable tracking control with saturation , 1995 .
[40] R. A. Hess,et al. Accommodating a Class of Actuator Failures in Flight Control Systems , 2000 .
[41] John Kaneshige,et al. Intelligent Control Approaches for Aircraft Applications , 2001 .
[42] Youmin Zhang,et al. Design of proportional-integral reconfigurable control systems via eigenstructure assignment , 2000, Proceedings of the 2000 American Control Conference. ACC (IEEE Cat. No.00CH36334).
[43] Mario G. Perhinschi,et al. Online parameter estimation issues for the NASA IFCS F-15 fault tolerant systems , 2002, Proceedings of the 2002 American Control Conference (IEEE Cat. No.CH37301).
[44] Daniel P. Schrage,et al. An open platform for reconfigurable control , 2001 .
[45] Eric N. Johnson,et al. Adaptive Guidance and Control for Hypersonic Vehicles , 2006 .
[46] John A. M. Petersen,et al. Interior-Point Algorithms for Control Allocation , 2003 .
[47] David J Smith,et al. Reliability, Maintainability and Risk: Practical Methods for Engineers , 1993 .
[48] Ilkay Yavrucuk,et al. Simulation of reconfigurable Heli-UAV's using main rotor RPM control in failure modes , 1999 .
[49] Kevin A. Wise,et al. DIRECT ADAPTIVE RECONFIGURABLE FLIGHT CONTROL FOR A TAILLESS ADVANCED FIGHTER AIRCRAFT , 1999 .
[50] Youdan Kim,et al. Partial eigenstructure assignment algorithm in flight control system design , 1999 .
[51] P. Antsaklis,et al. On the stability of the pseudo-inverse method for reconfigurable control systems , 1989, Proceedings of the IEEE National Aerospace and Electronics Conference.
[52] R. H. Miller,et al. Optimal fault detection and isolation filters for flight vehicle performance monitoring , 2003, 2003 IEEE Aerospace Conference Proceedings (Cat. No.03TH8652).
[53] Eugene A. Morelli,et al. Real-Time Stability and Control Derivative Extraction From F-15 Flight Data , 2003 .
[54] Meir Pachter,et al. Maneuvering Flight Control , 1998 .
[55] Meir Pachter,et al. Linear Regression with Intercept , 2004 .
[56] L. Zadeh,et al. On optimal control and linear programming , 1962 .
[57] R. Enns,et al. Helicopter flight control design using a learning control approach , 2000, Proceedings of the 39th IEEE Conference on Decision and Control (Cat. No.00CH37187).
[58] Eric N. Johnson,et al. Adaptive Trajectory Control for Autonomous Helicopters , 2005 .
[59] Kevin A. Wise,et al. Flight testing of a reconfigurable flight control law on the X-36 tailless fighter aircraft , 2000 .
[60] David B. Doman,et al. Dynamic inversion-based adaptive/reconfigurable control of the X-33 on ascent , 2001, 2001 IEEE Aerospace Conference Proceedings (Cat. No.01TH8542).
[61] D. P. Schrage,et al. Software-enabled control for intelligent UAVs , 1999, Proceedings of the 1999 IEEE International Symposium on Computer Aided Control System Design (Cat. No.99TH8404).
[62] Anthony J. Calise,et al. Development of a Reconfigurable Flight Control Law for Tailless Aircraft , 2001 .
[63] Bernard Mettler,et al. Nonlinear model for a small-size acrobatic helicopter , 2001 .
[64] Youmin Zhang,et al. Fault tolerant control system design with explicit consideration of performance degradation , 2003 .
[65] S. Sastry,et al. Adaptive Control: Stability, Convergence and Robustness , 1989 .
[66] Liang Tang,et al. From mission planning to flight control of unmanned aerial vehicles: Strategies and implementation tools , 2005, Annu. Rev. Control..
[67] Eric N. Johnson,et al. Adaptive Flight Control for an Autonomous Unmanned Helicopter , 2002 .
[68] Anthony J. Calise,et al. Multilayer neural network and adaptive nonlinear control of agile anti-air missiles , 1997 .
[69] M. Pachter,et al. RECONFIGURABLE FLIGHT CONTROL ON SLIDING MODES ADDRESSING ACTUATOR DEFLECTION AND DEFLECTION RATE SATURATION , 1998 .
[70] P. Antsaklis,et al. Stability of the pseudo-inverse method for reconfigurable control systems , 1991 .
[71] Anthony J. Calise,et al. Adaptive limit detection and avoidance for carefree maneuvering , 2001 .
[72] Jovan D. Boskovic,et al. A multiple model-based reconfigurable flight control system design , 1998, Proceedings of the 37th IEEE Conference on Decision and Control (Cat. No.98CH36171).
[73] D. G. Ward,et al. A self-designing receding horizon optimal flight controller , 1995, Proceedings of 1995 American Control Conference - ACC'95.
[74] David G. Ward,et al. Intelligent Control of Unmanned Air Vehicles: Program Summary and Representative Results , 2003 .
[75] Mario G. Perhinschi,et al. On-Line Parameter Estimation Issues for the NASA IFCS F-15 Fault Tolerant Systems , 2002 .