Robust partial integrated guidance and control of interceptors in terminal phase

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2009, Pages

  Das, Priya G ^a,b   Chawla, Charu ^a,b   Padhi, Radhakant ^a,b  

^a INDIAN INSTITUTE OF SCIENCE   (India)

^b Dept of Aerospace Engineering ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE DESIGNS; COMPUTATIONALLY EFFICIENT; DEVELOPED MODEL; DYNAMIC INVERSION; INNER LOOPS; INTEGRATED GUIDANCE; INTELLIGENT MANIPULATION; LOOP DESIGN; NONLINEAR DYNAMIC INVERSION; NUMERICAL RESULTS; OPTIMAL CONTROL THEORY; OPTIMAL CONTROLS; OUTER LOOP; PERFORMANCE ROBUSTNESS; ROLL RATES; ROTATIONAL DYNAMICS; SIMULATION STUDIES; SIX-DEGREE OF FREEDOMS; SIX-DOF; STABILIZATION LOOP; TIME SCALE SEPARATION; TIME-SCALES; TRANSLATIONAL MOTIONS; YAW RATE;

CONTROL; DESIGN; NAVIGATION; ONTOLOGY; OPTIMIZATION; TIME MEASUREMENT;

MODEL PREDICTIVE CONTROL;

EID: 78049239551     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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