Nonlinear prefilter to prevent pilot-induced oscillations due to actuator rate limiting

Journal of Guidance, Control, and Dynamics

Volumn 25, Issue 4, 2002, Pages 740-747

  Liebst, Brad S ^a   Chapa, Michael J ^a   Leggett, David B ^a  

^a AIR FORCE INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; CLOSED LOOP CONTROL SYSTEMS; COMPUTER SIMULATION; FEEDBACK CONTROL; FLIGHT DYNAMICS; OSCILLATIONS;

PILOT-INDUCED OSCILLATIONS (PIO);

NONLINEAR FILTERING;

EID: 0036641308     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4941     Document Type: Article

References (9)

1. Handling criteria
2. An alternate control scheme for alleviating aircraft-pilot coupling
3. Flight control system design and rate saturating actuators
4. Robust decoupled, flight control design with rate-saturating actuators