Compound control system design with direct thrust and aerodynamic force for air defence missile

Yuhang Xuebao/Journal of Astronautics

Volumn 29, Issue 6, 2008, Pages 1895-1900

  Zhu, Long Kui ^a   Tang, Guo Jian ^a   Yu, Meng Lun ^b  

^a NATIONAL UNIVERSITY OF DEFENSE TECHNOLOGY   (China)

^b Academy of China Aerospace Times Electronics Corporation   (China)

Author keywords

Air defense missile; Compound control; Linear quadratic optimal tracking control; Separation theory

Indexed keywords

AERODYNAMICS; AIR; AUTOMATION; CONTROL THEORY; GAS DYNAMICS; MISSILES; NAVIGATION; OBSERVABILITY; SEPARATION; SIGNAL PROCESSING;

AERODYNAMIC FORCES; AIR DEFENCES; AIR DEFENSE MISSILE; ATTITUDE STABILIZATIONS; BALLISTIC TARGETS; COMPOUND CONTROL; COUPLING EFFECTS; GUIDANCE COMMANDS; KINETIC ENERGY INTERCEPTORS; LINEAR QUADRATIC OPTIMAL TRACKING CONTROL; MANEUVERING TARGETS; MISS DISTANCES; MOTION MODELS; REFERENCE SIGNALS; RESPONSE TIMES; SIMULATION RESULTS; STATE OBSERVERS; STATE SPACE MODELS;

CONTROL SYSTEMS;

EID: 57949108337     PISSN: 10001328     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

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