An adaptive reconfigurable formation flight control design

In this paper we derive adaptive reconfigurable formation control algorithms using a leader-follower framework in the presence of loss-of-effectiveness control effector failures in the follower vehicle. We first present stable formation control algorithms designed to maintain the relative distances between the vehicles close to their desired values. A baseline reconfigurable control algorithm, and an online failure detection and identification system is then designed. Next, the adaptive reconfigurable control scheme is presented, followed by a proof of stability of the overall closed-loop formation control system. Simulation results are included to illustrate the properties of the proposed approach.

[1]  R. Mehra,et al.  Multiple-Model Adaptive Flight Control Scheme for Accommodation of Actuator Failures , 2002 .

[2]  Raman K. Mehra,et al.  A Hybrid Fault-Tolerant Scheme for Flight Control Applications* , 2001 .

[3]  M. Pachter,et al.  Optimal formation flight control , 1996 .

[4]  Rajeeva Kumar,et al.  Adaptive control of UAVs in close-coupled formation flight , 2000, Proceedings of the 2000 American Control Conference. ACC (IEEE Cat. No.00CH36334).

[5]  Petros A. Ioannou,et al.  Accommodation of failures in the F-16 aircraft using adaptive control , 1991, IEEE Control Systems.

[6]  Mario Innocenti,et al.  Preliminary analysis of formation flight management , 1999 .

[7]  Jovan D. Boskovic,et al.  Intelligent Adaptive Control of a Tailless Advanced Fighter Aircraft Under Wing Damage , 2000 .

[8]  Michael Veth,et al.  Energy preserving formation flight control , 1995 .

[9]  Mark R. Anderson,et al.  FORMATION FLIGHT AS A COOPERATIVE GAME , 1998 .

[10]  Seungjae Lee,et al.  Direct adaptive reconfigurable control of a tailless fighter aircraft , 1998 .

[11]  M. Pachter,et al.  Automatic formation flight control , 1992 .

[12]  Jovan D. Boskovic,et al.  Stable multiple model adaptive flight control for accommodation of a large class of control effector failures , 1999, Proceedings of the 1999 American Control Conference (Cat. No. 99CH36251).

[13]  Meir Pachter,et al.  Adaptive feedback linearizing nonlinear close formation control of UAVs , 2000, Proceedings of the 2000 American Control Conference. ACC (IEEE Cat. No.00CH36334).

[14]  Kumpati S. Narendra,et al.  Adaptive control using multiple models , 1997, IEEE Trans. Autom. Control..

[15]  Kevin A. Wise,et al.  DIRECT ADAPTIVE RECONFIGURABLE FLIGHT CONTROL FOR A TAILLESS ADVANCED FIGHTER AIRCRAFT , 1999 .

[16]  Sai-Ming Li,et al.  Semi-globally stable formation flight control design in three dimensions , 2001, Proceedings of the 40th IEEE Conference on Decision and Control (Cat. No.01CH37228).

[17]  Sai-Ming Li,et al.  Evaluation of the properties of a multiple-model reconfigurable flight controller on a 6 DOF simulation , 2000 .

[18]  Sai-Ming Li,et al.  GLOBALLY STABLE AUTOMATIC FORMATION FLIGHT CONTROL IN TWO DIMENSIONS , 2001 .

[19]  John D'Azzo,et al.  Close formation flight control , 1999 .

[20]  Meir Pachter,et al.  Input-output Invertibility and Sliding Mode Control for Close Formation Flying of Multiple UAVS , 2000 .

[21]  R. K. Mehra,et al.  Multiple model-based adaptive reconfigurable formation flight control design , 2002, Proceedings of the 41st IEEE Conference on Decision and Control, 2002..

[22]  Wright-Patterson Afb,et al.  Input-Output Invertibility and Sliding Mode Control for Close Formation Flying * , 2000 .

[23]  Meir Pachter,et al.  System identification for adaptive and reconfigurable control , 1995 .

[24]  Marc Bodson,et al.  Multivariable adaptive algorithms for reconfigurable flight control , 1997, IEEE Trans. Control. Syst. Technol..

[25]  Meir Pachter,et al.  Formation maneuvers in three dimensions , 2000, Proceedings of the 39th IEEE Conference on Decision and Control (Cat. No.00CH37187).

[26]  Vincent P Reyna Automation of Formation Flight Control , 1994 .