Stabilization of a solid propellant rocket instability

Proceedings of the IEEE Conference on Decision and Control

Volumn 5, Issue , 2001, Pages 4483-4488

  Bošković, Dejan M ^a   Krstić, Miroslav ^a  

^a UNIVERSITY OF CALIFORNIA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

APPROXIMATION THEORY; ASYMPTOTIC STABILITY; BOUNDARY CONDITIONS; CONTROL SYSTEM SYNTHESIS; FINITE DIFFERENCE METHOD; MATHEMATICAL MODELS; NONLINEAR EQUATIONS; ORDINARY DIFFERENTIAL EQUATIONS; PARTIAL DIFFERENTIAL EQUATIONS; ROCKET ENGINES; SOLID PROPELLANTS; SYSTEM STABILITY;

BACKSTEPPING DESIGN; FINITE DIFFERENCE APPROXIMATION;

FEEDBACK CONTROL;

EID: 0035708422     PISSN: 01912216     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (11)

1. Backstepping in infinite dimension for a class of parabolic distributed parameter systems
2. Nonlinear stabilization of a thermal convection loop by state feedback
3. Robust control of parabolic PDE systems with time-dependent spatial domains
4. A review of calculations for unsteady burning of a solid propellant
5. A simplified model of unstable burning in solid propellants
6. Unsteady thermal response of the condensed-phase fuel adjacent to a reacting boundary layer
7. Quasi-steady gas-phase flame theory in unsteady burning of a homogeneous solid propellant