Flight test validation of sideslip estimation using inertial accelerations

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2000, Pages

  Colgren, Richard D ^a   Martin, Keith E ^b  

^a UNIVERSITY OF PHOENIX   (United States)

^b Lockheed Martin Aeronautics Company   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; ANGLE OF ATTACK; ANGLE OF ATTACK INDICATORS;

AIRCRAFT FLIGHT TESTS; AVIONICS SYSTEMS; FLIGHT TEST; SIDESLIP ANGLES;

AIR NAVIGATION;

EID: 85088758828     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-4448     Document Type: Conference Paper

References (3)

1. Colgren, Richard D., Frye, Michael T. and Olson, Wayne M., "A Proposed System Architecture For Estimation Of Angle-Of-Attack And Sideslip Angle." Presented at the AIAA Guidance, Navigation, and Control Conference, August 1999.
2. Colgren, Richard D., "The Feasibility of Using an INS for Control System Feedbacks." Presented at the World Aviation Congress and Exposition, September 1998.
3. Colgren, Richard D., "Results of the U-2 Autopilot and Air Data System (APADS) Development and Flight Test Program." Presented at the AIAA Guidance, Navigation, and Control Conference, August 1996.