PIO analysis with actuator rate limiting

21st Atmospheric Flight Mechanics Conference

Volumn , Issue , 1996, Pages 569-580

  Klyde, David H ^a   McRuer, Duane T ^a   Myers, Thomas T ^a  

^a SYSTEMS TECHNOLOGY INC   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DESCRIBING FUNCTIONS; RESEARCH AIRCRAFT; SUPERSONIC AIRCRAFT;

ACTUATOR DESIGN; ANALYSIS TECHNIQUES; BANDWIDTH REDUCTIONS; MAGNITUDE REDUCTION; PILOT-INDUCED OSCILLATIONS; RATE LIMITING; RATE-LIMITED ACTUATORS; SIMULATION TECHNIQUE;

ACTUATORS;

EID: 84983103195     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-3432     Document Type: Conference Paper

References (9)

1. Ashkenas Irving L., Henry R. Jex, and Duane T. McRuer, Pilot-Induced Oscillations: Their Causes and Analysis, Northrop-Norair Rept., NOR 64-143, June 1964.
2. Hanke, Dietrich, "Handling Qualities Analysis on Rate Limiting Elements in Flight Control Systems," Flight Vehicle Integration Panel Workshop on Pilot Induced Oscillations, AGARD-AR-335, Feb. 1995.
3. Duda, H., Frequency Domain Analysis of Rate Limiting elements in Flight Control Systems, DLR-FB 94-16, Braunschweig, 1994. (In German).
4. Klyde, David H., Duane T. McRuer, and Thomas T. Myers, Unified Pilot-Induced Oscillation Theory Volume 1: PIO Analysis with Linear and Nonlinear Effective Vehicle Characteristics, Including Rate Limiting, WL-TR-96-3028, Dec. 1995.
5. McRuer, Duane T., Pilot-Induced Oscillations and Human Dynamic Behavior, NASA CR-4683, July 1995.
6. Graham, Dunstan and Duane McRuer, Analysis of Nonlinear Control Systems, John Wiley and Sons, Inc., New York, 1961, (Also Dover, 1971).
7. Matranga, Gene J., Analysis of X-I5 Landing Ap proach and Flare Characteristics Determined from the First 30 Flights, NASA TN D-1057, July 1961.
8. Heffley, Robert K., and Wayne F, Jewell, Aircraft Handling Qualities Data, NASA CR-2144, Dec. 1972.
9. Taylor, Lawrence W., Jr., and John W. Smith, An Analysis of the Limit-Cycle and Structural-Resonance Characteristics of the X-15 Stability Augmentation System, NASA TN D-4287, Dec. 1967.