Design and validation of flight control law changes intended to minimize pilot-induced oscillations in a large transport aircraft

Collection of Technical Papers - AIAA Atmospheric Flight Mechanics Conference

Volumn 1, Issue , 2005, Pages 112-116

  Shweyk, Kamal M ^a,b   Weltz, Gary L ^a,b  

^a BOEING COMPANY   (United States)

^b AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL LAWS; FEEDBACK GAINS; PILOT-INDUCED OSCILLATION (PIO); SIMULATION TESTS;

AIRCRAFT; COMPUTER SIMULATION; CONTROL THEORY; MANEUVERABILITY; OSCILLATIONS; SIMULATORS;

FLIGHT DYNAMICS;

EID: 29344453621     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)

1. Iloputaife, O. "Minimizing Pilot-Induced Oscillation Susceptibility During C-17 Development," AIAA 97-3497, 1997
2. Shweyk, K.M. et al. "C-17 Roll PIO Non-Advocate Review Presentation," Boeing Internal Document, Long Beach, California, April 1-2, 2003.
3. Black, T., Lee, B.P., and Hoh, R.H. "C-17 Roll PIO Non-Advocate Review Team Report," Boeing Memorandum C17-FCS-MDA-03-010, Long Beach, California, April 28, 2003.
4. Rossitto, K.F., von Klein, W.T., Armor, J. "C-17 Roll Axis Pilot Induced Oscillation Baseline and Proposed Change Analysis, Final Report" Boeing Report 04H0054, Huntington Beach, California, March 8, 2004.
5. Shweyk K.M. and Rossitto K.F. "Proposed Roll Control Criteria for the Design of Lateral Control Stick Shaping Functions in large Transport Aircraft," AIAA 99-4094, Atmospheric Flight Mechanics Conference, Portland, Oregon, August 9-11, 1999.\
6. Mitchell, D.G., Arencibia, A.J., "Real-Time Detection of Pilot-Induced Oscillations," AIAA 2004-4700, Atmospheric Flight Mechanics Conference, Providence, Rhode Island, 19 August 2004.