Nonlinear control design of a hypersonic aircraft using sum-of-squares method

Proceedings of the American Control Conference

Volumn , Issue , 2007, Pages 5278-5283

  Ataei Esfahani, Armin ^b   Qian, Wang ^a,b  

^a IEEE

^b PENNSYLVANIA STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC COEFFICIENTS; APPLIED (CO); CONTROL DESIGNS; DEFLECTION (OVALIZATION); DUAL PROBLEMS; FAST DYNAMICS; HYPERSONIC AIRCRAFT; LONGITUDINAL DYNAMICS; LYAPUNOV; LYAPUNOV THEOREMS; NON-LINEAR CONTROLLERS; NON-LINEAR DYNAMICS; NONLINEAR CONTROL DESIGN; PARAMETER UNCERTAINTIES; PITCH RATE; SEMI-DEFINITE PROGRAMS (SDP); SIMULATION RESULTS; SLOW DYNAMICS (SD); SOS TECHNIQUE; SUM OF SQUARES (SOS); TIME SCALE DECOMPOSITION; TIME SCALING;

AIRCRAFT; CONTROL THEORY; DIFFERENTIAL EQUATIONS; GAS DYNAMICS; LYAPUNOV FUNCTIONS; MILITARY DATA PROCESSING; ROBUST CONTROL; ROBUSTNESS (CONTROL SYSTEMS); SEMICONDUCTOR SWITCHES; TELECOMMUNICATION NETWORKS;

DYNAMICS;

EID: 44449137519     PISSN: 07431619     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/ACC.2007.4282934     Document Type: Conference Paper

References (8)

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8. A. Ataei-Esfahani, "Robust control design for aircrafts: Case studies using semidefinite programming approaches," Master's thesis, Penn State University, 2006.