Integrated guidance/autopilot design for missiles with impact angle constraints

Proceedings of IEEE ICIA 2006 - 2006 IEEE International Conference on Information Acquisition

Volumn , Issue , 2006, Pages 75-79

  Xu, Qingjiu ^a   Yu, Jiandong ^a   Yu, Jinyong ^a   Yang, Xiuzhen ^a  

^a NAVAL AERONAUTICAL AND ASTRONAUTICAL UNIVERSITY   (China)

Author keywords

[No Author keywords available]

Indexed keywords

MERGERS AND ACQUISITIONS; MISSILES; ORDNANCE;

(E ,2E) THEORY; BACKSTEPPING; HIGH ACCURACY; IMPACT ANGLES; INFORMATION ACQUISITIONS; INTEGRATED DESIGNS; INTEGRATED GUIDANCE/AUTOPILOT DESIGN; INTERNATIONAL CONFERENCES; MANEUVERING TARGETS; SIMULATION RESULTS; YAW PLANE;

MILITARY EQUIPMENT;

EID: 46249104254     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/ICIA.2006.305835     Document Type: Conference Paper

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