A control allocation system for automatic detection and compensation of phase shift due to actuator rate limiting

This paper proposes a control allocation system that can detect and compensate the phase shift between the desired and the actual total control effort due to rate limiting of the actuators. Phase shifting is an important problem in control system applications since it effectively introduces a time delay which may destabilize the closed loop dynamics. A relevant example comes from flight control where aggressive pilot commands, high gain of the flight control system or some anomaly in the system may cause actuator rate limiting and effective time delay introduction. This time delay can instigate Pilot Induced Oscillations (PIO), which is an abnormal coupling between the pilot and the aircraft resulting in unintentional and undesired oscillations. The proposed control allocation system reduces the effective time delay by first detecting the phase shift and then minimizing it using constrained optimization techniques. Flight control simulation results for an unstable aircraft with inertial cross coupling are reported, which demonstrate phase shift minimization and recovery from a PIO event.

[1]  Ola Härkegård,et al.  Backstepping and control allocation with applications to flight control , 2003 .

[2]  Yildiray Yildiz,et al.  A control allocation technique to recover from pilot-induced oscillations (capio) due to actuator rate limiting , 2010, Proceedings of the 2010 American Control Conference.

[3]  Michael J. Chapa A Nonlinear Pre-Filter to Prevent Departure and/or Pilot-Induced Oscillations (PIO) Due to Actuator Rate Limiting , 1999 .

[4]  David G. Mitchell,et al.  Investigating The Role of Rate Limiting in Pilot-Induced Oscillations , 2003 .

[5]  P. R. Deppe,et al.  Flight Evaluation of an Aircraft with Side and Center Stick Controllers and Rate-Limited Ailerons , 1996 .

[6]  D. Hanke,et al.  Phase compensation: a means of preventing aircraft-pilot coupling caused by rate limitation , 1998 .

[7]  David Leggett,et al.  Nonlinear Prefilter to Prevent Pilot-Induced Oscillations due to Actuator Rate Limiting , 2002 .

[8]  Wayne C. Durham,et al.  MULTIPLE CONTROL EFFECTOR RATE LIMITING , 1995 .

[9]  D. Hanke,et al.  Handling Qualities Analysis on Rate Limiting Elements in Flight Control Systems. , 1994 .

[10]  Lars Rundqwist,et al.  Phase compensation of rate limiters in JAS 39 Gripen , 1996 .

[11]  D. Enns CONTROL ALLOCATION APPROACHES , 1998 .

[12]  Marc Bodson,et al.  Evaluation of optimization methods for control allocation , 2001 .

[13]  Ralph A'Harrah An alternate control scheme for alleviating aircraft-pilot coupling , 1994 .

[14]  David G. Mitchell,et al.  Real-Time Detection of Pilot-Induced Oscillations , 2004 .

[15]  Ronald A. Hess,et al.  Flight control system design with rate saturating actuators , 1996 .

[16]  Ronald A. Hess,et al.  Robust, Decoupled, Flight Control Design with Rate-Saturating Actuators , 1998 .

[17]  Torkel Glad,et al.  Resolving actuator redundancy - optimal control vs. control allocation , 2005, Autom..