Model based IVHM System for the Solid Rocket Booster

IEEE Aerospace Conference Proceedings

Volumn , Issue , 2008, Pages

  Luchinsky, Dmitry G ^a   Osipov, Vyatcheslav V ^b   Smelyanskiy, Vadim N ^a   Timucin, Dogan A ^a   Uckun, Serdar ^a  

^a NASA AMES RESEARCH CENTER   (United States)

^b MISSION CRITICAL TECHNOLOGIES INC   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANALYTICAL SOLUTIONS; CONSISTENT ALGORITHMS; CYLINDRICAL SYMMETRY; EXPERIMENTAL DATA; FAULT MODES; GAS FLOWING; HIGH-FIDELITY; HOT GAS FLOW; INFERENCE METHODS; INTERNAL BALLISTICS; METAL CASES; MODEL PARAMETERS; MODEL-BASED; NOZZLE THROAT; ONE-DIMENSIONAL; PERFORMANCE MODELLING; PROBABILISTIC APPROACHES; QUASI-ADIABATIC; QUASI-STATIONARY APPROXIMATIONS; REAL-TIME DIAGNOSTICS; SOLID ROCKET BOOSTERS; STOCHASTIC DIFFERENTIAL EQUATIONS;

ABLATION; AERODYNAMICS; AIRCRAFT ENGINES; ALGORITHMS; APPROXIMATION ALGORITHMS; COMBUSTION; COMBUSTION CHAMBERS; COMPUTATIONAL FLUID DYNAMICS; DIFFERENCE EQUATIONS; DIFFERENTIAL EQUATIONS; DIFFERENTIATION (CALCULUS); FLOW OF GASES; GAS DYNAMICS; HEALTH; INFERENCE ENGINES; LAW ENFORCEMENT; METAL MELTING; METALS; MILITARY APPLICATIONS; NOZZLES; PARAMETER ESTIMATION; PARTIAL DIFFERENTIAL EQUATIONS; POLYNOMIAL APPROXIMATION; ROCKETS; SMELTING; STOCHASTIC PROGRAMMING; STRAIN RELAXATION;

BOOSTERS (ROCKET);

EID: 49349087081     PISSN: 1095323X     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/AERO.2008.4526644     Document Type: Conference Paper

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