Analysis of the controlled NASA HL20 atmospheric re-entry vehicle based on dynamic IQCs

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2009, Pages

  Veenman, J ^a,b   Koroglu H ^a,b   Scherer, C W ^a,b  

^a DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

^b DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

CLOSED LOOP SYSTEMS; NASA; NONLINEAR EQUATIONS; REENTRY;

ATMOSPHERIC RE-ENTRY VEHICLES; COMPLEX APPLICATIONS; INTEGRAL QUADRATIC CONSTRAINTS; LINEAR FRACTIONAL REPRESENTATION; LINEAR-PARAMETER VARYING CONTROLLERS; PARAMETRIC UNCERTAINTIES; POLYNOMIAL INTERPOLATION; TIME-VARYING PARAMETRIC UNCERTAINTIES;

UNCERTAINTY ANALYSIS;

EID: 78049276855     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2009-5637     Document Type: Conference Paper

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