A Fault-Tolerant Control Architecture for Unmanned Aerial Vehicles

projects: Software Enabled Control (SEC), SEC Renegade (a follow-on to the SEC project funded to apply SEC technologies to a full-scale rotorcraft), and Heterogeneous Urban Reconnaissance, Surveillance, and Target Acquisition Team (HURT). My deepest thanks are for Professor George J. Vachtsevanos, who advised me through the completion of this work. His critical input, guidance, and mentoring have been invalu-Lastly, my wife Michelle contributed to every page in ways she does not even know. I could not have done it without her.

[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 .