A comparison of rate-limit compensation schemes for pilot-induced- oscillation avoidance

Aerospace Science and Technology

Volumn 10, Issue 1, 2006, Pages 37-47

  Gatley, Sarah L ^a   Turner, Matthew C ^a   Postlethwaite, Ian ^a   Kumar, Abhishek ^a  

^a UNIVERSITY OF LEICESTER   (United Kingdom)

Author keywords

Anti windup; Control; Fly by wire; PIO; Rate limit

Indexed keywords

AERODYNAMICS; AEROSPACE INDUSTRY; AIRCRAFT MODELS; COMPUTER SIMULATION; CONTROL SYSTEM ANALYSIS; NONLINEAR SYSTEMS; OSCILLATIONS;

ANTI-WINDUP; FLY-BY-WIRE; PIO; RATE-LIMIT;

ACTUATORS;

EID: 31044456947     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ast.2005.07.004     Document Type: Article

References (13)

1. G. Duus, H. Duda, Analysis of the have limits database using the OLOP criteria, in: AIAA Atmospheric Flight Mechanics Conference and Exhibit, Portland, Oregon, AIAA-99-4007, August 1999
2. G. Duus, lateral dynamics of F18 model, Private communication
3. C. Edwards, and I. Postlethwaite Anti-windup and bumpless transfer scheme Automatica 24 2 1998 199 210
4. E. Fillipone, PIO Toolbox (release 1), preliminary version released to AG-12 members
5. G.P. Gilbreath, Prediction of pilot-induced oscillations (PIO) due to actuator rate limiting using the open-loop onset point (OLOP) criterion, M. Sc. thesis, Air Force Institute of Technology, March 2001
6. G. Hovmark, Proposed ADMIRE test-matrix, Matrix of flight conditions and rate-limit values
7. G. Hovmark, G. Duus, Experimental evaluation of phase compensating rate limiters in an aircraft's lateral flight control system, Technical Report TP-120-04, GARTEUR, August 2000
8. I. Postlethwaite, M. Turner, E. Prempain, An H ∞ approach to rate-limit compensation for pilot-induced-oscillation avoidance: concept, demonstration and comparison, GARTEUR FM(AG12)/TP-120-06, March 2001
9. L. Rundquist, K. Stahl-Gunnarsson, Phase compensation of rate-limiters in unstable aircraft, in: IEEE Conference on Control Applications, 1996, pp. 19-24
10. R.E. Smith, Evaluation of F-18A approach and landing flying qualities using an in-flight simulator, Technical Report 6241-F-1, Calspan, 1979
11. M.C. Turner, D.J. Walker, and A.G. Alford Design and ground-based simulation of an H ∞ limited authority control system for the Westland Lynx helicopter Aerospace Science and Technology 5 2001 221 234
12. T. Wilmes, H. Duda, Investigation of electronic filters to prevent aircraft-pilot-coupling, Technical Report IB 111-98/29, Institut fur Flugmechanic, Braunschweig, November 1998
13. R. Van der Weerd Pilot-Induced Oscillation Suppression Methods and their Effects on Large Transport Aircraft Handling Qualities December 2000 Delft University Press