X-31 VECTOR - ESTOL to the ground flight test results and lessons learned

Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference

Volumn 3, Issue , 2004, Pages 1526-1539

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

^a AIRBUS GROUP INNOVATIONS   (Germany)

^b DLR Germnay ^*

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL LAWS; FLIGHT TEST; SINK RATES; TEST PHASES;

AIRCRAFT LANDING; AIRFRAMES; AUTOMATION; EQUIPMENT TESTING; INERTIAL NAVIGATION SYSTEMS; MANEUVERABILITY; MILITARY AIRCRAFT; OPTIMAL CONTROL SYSTEMS; ROBUSTNESS (CONTROL SYSTEMS);

AEROSPACE VEHICLES;

EID: 19944394888     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (4)

1. Beh, H., Van den Bunt, R., Fischer, B., High Angle of Attack Approach and Landing Control Law Design for the X-31 A,
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. Grohs, Fischer, Heinzinger, Brieger: X-31 VECTOR Control Law Design for ESTOL to the Ground, AIAA GNC Conference 2003
4. Selmon, J. et al: High Angle of Attack Autonomous Landing Using the X-31 A Aircraft, AIAA GNC Conference 2001