Derivation of zero-gravity structural control models from analysis and ground experimentation

Journal of Guidance, Control, and Dynamics

Volumn 19, Issue 4, 1996, Pages 787-793

  Glaese, Roger M ^a,b   Miller, David W ^a,b  

^a MASSACHUSETTS INSTITUTE OF TECHNOLOGY   (United States)

^b AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

CLOSED LOOP CONTROL SYSTEMS; COMPUTER SIMULATION; CONTROL EQUIPMENT; CONTROL SYSTEM SYNTHESIS; FINITE ELEMENT METHOD; FLIGHT DYNAMICS; MATHEMATICAL MODELS; MICROGRAVITY PROCESSING; PERTURBATION TECHNIQUES; PREDICTIVE CONTROL SYSTEMS; SPACE FLIGHT; SPACE SHUTTLES;

GROUND EXPERIMENTATION; MIDDECK ACTIVE CONTROL EXPERIMENT; SPACE SHUTTLE FLIGHT EXPERIMENT; STRUCTURAL PERTURBATION; SUSPENSION ASPECTS; ZERO GRAVITY STRUCTURAL CONTROL MODELS;

CONTROL THEORY;

EID: 0030190444     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/3.21700     Document Type: Article

References (12)

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