High angle of attack control law development and testing for the F/A-18E/F super hornet

1999 Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 1999, Pages 541-551

  Heller, Michael ^a   Niewoehner, Robert J ^b   Lawson, Kenneth P ^c  

^a BOEING COMPANY   (United States)

^b UNITED STATES NAVAL ACADEMY   (United States)

^c NAVAL AIR SYSTEMS COMMAND   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; SOFTWARE TESTING;

CONTROL LAWS; DESIGN HISTORY; DEVELOPMENT AND TESTING; ENGINEERING AND MANUFACTURING DEVELOPMENT; F/A-18 HORNET; FLIGHT TEST PROGRAMS; HIGH ANGLE OF ATTACK; INITIAL DESIGN;

FIGHTER AIRCRAFT;

EID: 78049305153     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-4051     Document Type: Conference Paper

References (4)

1. For example, see any of dozens of papers published in High Angle ofAttack Technology Conference Proceedings, NASA Conference Publications CP-3149 (1990) or CP-3137 (1992).
2. Traven, Madenwald, Heller, Hoffman, "Enhanced High AOA Agility and Spin Recovery for the F/A-18E/F Super Hornet, " SETP European Symposium, May, 1999.
3. Foster, John, "Investigation of the Susceptibility of Fighter Airplanes to the Out-of-Control Falling Leaf Mode, " High Angle of Attack Technology Conference Proceedings, NASA Conference Publications CP-1998-207676/PT2, June, 1998, pg. 601-639.
4. Madenwald, Niewoehner and Hoy, "F/A-18 E/F High AOA Flight Test Development Program, " SETP 1998 Report to the Aerospace Profession: Proceedings, September, 1998, pg. 128-142.