X-31 VECTOR control law design for ESTOL to the ground

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2003, Pages

  Grohs, T ^a,b   Fischer, Balazs ^a,b   Heinzinger, Olaf ^a,b   Brieger, Oliver ^a,b  

^a AIRBUS GROUP INNOVATIONS   (Germany)

^b GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL LAWS; FLIGHT MANEUVERS; GROUND PHASE; HIGH ANGLES OF ATTACK; NAVAL AIR STATION; RELIABILITY AND ROBUSTNESS; SHORT TAKE-OFF AND LANDINGS; VECTOR CONTROLS;

FLIGHT CONTROL SYSTEMS; LANDING;

CONTROL THEORY;

EID: 84896852701     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (3)

1. Beh, H., Van den Bunt, R., Fischer, B., High Angle of Attack Approach and Landing Control Law Design for the X-31A,
2. Beh, H.; Hofinger, G.: Control Law Design of the Experimenal Aircraft X-31A, ICAS-94- 7.2.1, ICAS Proceedings 1994, Anaheim, California, USA
3. Selmon, J. et al: High Angle of Attack Autonomous Landing Using the X-31A Aircraft, AIAA GNC Conference 2001