Application of new and standard Pilot-Induced Oscillation (PIO) analysis methods to flight test data of the C-17 transport aircraft

AIAA Atmospheric Flight Mechanics Conference

Volumn 1, Issue , 2007, Pages 266-291

  Weltz, Gary L ^a   Shweyk, Kamal M ^a   Murray, David M ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT CONTROL; CONTROL THEORY; DYNAMICS; LANDING; STOCHASTIC SYSTEMS; TRANSPORT AIRCRAFT; AIRCRAFT; BANDWIDTH; PROBLEM SOLVING; STOCHASTIC CONTROL SYSTEMS;

ANALYTICAL METHOD; APPROACH AND LANDINGS; FLIGHT CONDITIONS; FLIGHT TEST DATA; FLIGHT TEST EVALUATION; GLOBEMASTER III; OSCILLATORY DYNAMICS; PILOT-INDUCED OSCILLATIONS; PILOT MODEL METHOD; PILOT-INDUCED OSCILLATION (PIO);

TIME DOMAIN ANALYSIS; FLIGHT DYNAMICS;

EID: 40549092653     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. Iloputaife, O. "Minimizing Pilot-Induced Oscillation Susceptibility During C-17 Development," AIAA 97-3497, AIAA Atmospheric Flight Mechanics Conference, New Orleans, LA, August 11-13, 1997
2. Shweyk, K.M, Weltz, G.L. "Design and Validation of Flight Control Law Changes Intended to Minimize Pilot-Induced oscillations in a Large Transport Aircraft," AIAA 2005-5812, AIAA Atmospheric Flight mechanics Conference, San Francisco, California, August 15-18 2005.
3. 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.
4. 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.
5. Mitchell, D.G., "Application of ROVER to Boeing-Supplied Time Histories Under P.O. No. 2CS0527," Hoh Aeronautics, Inc. Memorandum, Lomita, California, 18 December 2002.