Control of commercial aircraft with vertical tail loss

Collection of Technical Papers - AIAA 4th Aviation Technology, Integration, and Operations Forum, ATIO

Volumn 1, Issue , 2004, Pages 347-357

  Crider, Leah D ^a  

^a GE GLOBAL RESEARCH   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT CONTROLLER DESIGN; AIRLINERS; FAULT DETECTION SYSTEM; RUDDER MOVEMENTS;

AIRCRAFT; AIRCRAFT LANDING SYSTEMS; CONTROL EQUIPMENT; EQUATIONS OF MOTION; MATHEMATICAL MODELS; MATRIX ALGEBRA; VELOCITY MEASUREMENT;

EMPENNAGES;

EID: 19644395097     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. National Transportation Safety Board. NTSB DCA97MA049 and CDA02MA001.
2. rd ed., John Wiley & Sons, New York, 1996. App. B, E.
3. Stengel, Robert F. Aircraft Flight Dynamics (to be published), Chaps. 1-6, Eq. 4.1-100 and 4.1-101.
4. McLean, Donald. Automatic Flight Control Systems, Prentice Hall, New York, 1990, p. 34, 159-61
5. Martinelli, Luigi. "MAE 332: Aircraft Design," Princeton University, Princeton, 2003.
6. Stengel, Robert F. Optimal Control and Estimation, Dover Publications, New York, 1986. Chap. 6.
7. "Flight Control Systems - Design, Installation, and Test of Piloted Aircraft, General Specifications for," U.S. DOD MIL-F-9490D, Washington, DC. 3.1.2
8. "Flying Qualities of Piloted Airplanes," U.S. DOD MIL-F-8785C, 1980, 3.3.1.4