The problem of on-line digital computer control of the NERVA nuclear rocket engine is considered. Proposed is a method of State Dependent State Variable Feedback (SDSVF) as a practical approach to the control of NERVA and other complex nonlinear and/or time-varying systems. The difficulties inherent in other design methods are avoided by defining the optimal closed loop system in terms of a desired transfer function, rather than a performance index to maximize or minimize
Digital computer program based on matrix formulation for analysis and design of linear state variabl...
Second Method of Liapunov, Popov frequency criterion, and matrix inequality method used to study sta...
Fuel sloshing and rigid body oscillations in large rocket booster control during launchin
Linear optimal feedback control theory for nuclear rocket dynamics and control problem
State variable feedback design of control system for coupled core nuclear reacto
In a nuclear thermal rocket engine, the propellant gas can be varied independent of the peak chamber...
The thermionic reactor control system design studies conducted over the past several years for a nuc...
Automatic control theory applied to nuclear rocket dynamics and control using stochastic algorithm
The control of an airbreathing turbojet engine by an onboard digital computer is studied. The approa...
Linear and nonlinear control systems via state variable feedback with applications in nuclear reacto...
Specifications, sensitivity, intentional nonlinearities, and unavailable states concerned with state...
Using nonlinear digital simulation as a representative model of the dynamic operation of the QCSEE t...
Flight weight digital computers are being used today to carry out many of the propulsion system cont...
This thesis shows that reaction jet thrust pulses, each of constant amplitude and time duration, in ...
The topics are presented in viewgraph form and include the following: systems approach needed for nu...
Digital computer program based on matrix formulation for analysis and design of linear state variabl...
Second Method of Liapunov, Popov frequency criterion, and matrix inequality method used to study sta...
Fuel sloshing and rigid body oscillations in large rocket booster control during launchin
Linear optimal feedback control theory for nuclear rocket dynamics and control problem
State variable feedback design of control system for coupled core nuclear reacto
In a nuclear thermal rocket engine, the propellant gas can be varied independent of the peak chamber...
The thermionic reactor control system design studies conducted over the past several years for a nuc...
Automatic control theory applied to nuclear rocket dynamics and control using stochastic algorithm
The control of an airbreathing turbojet engine by an onboard digital computer is studied. The approa...
Linear and nonlinear control systems via state variable feedback with applications in nuclear reacto...
Specifications, sensitivity, intentional nonlinearities, and unavailable states concerned with state...
Using nonlinear digital simulation as a representative model of the dynamic operation of the QCSEE t...
Flight weight digital computers are being used today to carry out many of the propulsion system cont...
This thesis shows that reaction jet thrust pulses, each of constant amplitude and time duration, in ...
The topics are presented in viewgraph form and include the following: systems approach needed for nu...
Digital computer program based on matrix formulation for analysis and design of linear state variabl...
Second Method of Liapunov, Popov frequency criterion, and matrix inequality method used to study sta...
Fuel sloshing and rigid body oscillations in large rocket booster control during launchin