Full envelope missile autopilot design using gain scheduled robust control

Journal of Guidance, Control, and Dynamics

Volumn 22, Issue 1, 1999, Pages 115-122

  Buschek, Harald ^a,b  

^a BGT Bodenseewerk Geratetechnik GmbH   (Germany)

^b AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE; AUTOMATION; COMPUTER SIMULATION; CONTROL SYSTEM SYNTHESIS; LINEAR CONTROL SYSTEMS; MATHEMATICAL MODELS; MISSILES; ROBUSTNESS (CONTROL SYSTEMS); VIBRATIONS (MECHANICAL);

FULL FLIGHT ENVELOPE CONTROL; MISSILE AUTOPILOTS;

ELECTRONIC GUIDANCE SYSTEMS;

EID: 0032785313     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4357     Document Type: Article

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