A new approach to attitude stability and control for low airspeed vehicles

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

Volumn 2, Issue , 2004, Pages 1268-1283

  Lim, K B ^a,b   Shin, J Y ^a,c   Moerder, D D ^a,b   Cooper, E G ^a,d  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b Guidance and Control Branch   (United States)

^c NATIONAL INSTITUTE OF AEROSPACE   (United States)

^d Systems Integration Branch   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; CONTROL EQUIPMENT; CONTROL SYSTEM ANALYSIS; FLIGHT DYNAMICS; NONLINEAR CONTROL SYSTEMS; SYSTEM STABILITY; TORQUE; VECTORS;

AIRSPEED VEHICLES; ANGULAR MOMENTUM (AM); ATTITUDE STABILITY; THRUST-LEVITATED VEHICLES;

AIRFRAMES;

EID: 19744375853     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-5008     Document Type: Conference Paper

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