Add to ORKGWeighted least squares parameter estimation, Kalman filter, and random search problems for aerospace guidance control system desig
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1998.Includes...
Integrated engine-airframe optimal control technology may significantly improve aircraft performance...
Design method including effects of parameter uncertainties in design of linear control system
The first twelve system state variables are presented with the necessary mathematical developments f...
Progress reports on guidance and attitude control mechanisms of different flight vehicles are presen...
Data smoothing technique for parameter optimization in free flight orbit vehicle-borne tracking syst...
Least squares method for sequential guidance estimates on ballistic vehicle in partially known atmos...
Application of quadratic optimal control, least squares state, and parameter estimation to stability...
As a unified extension of a group of related mathematical procedures, Kalman filtering is of assista...
Thesis (Sc. D.)--Massachusetts Institute of Technology, Dept. of Aeronautical Engineering, 1967.Vita...
Control system optimization for Saturn 5 launch vehicles using gradient technique
This dissertation studies guidance and control of aerospace systems. Guidance algorithms are used to...
Research of control optimization, stochastic stability, and air traffic control problem
Research on flight control systems is reviewed. Investigations were conducted to evaluate and test a...
Least squares, minimum variance, and Kalman estimation applied to mathematical model of free flight ...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1998.Includes...
Integrated engine-airframe optimal control technology may significantly improve aircraft performance...
Design method including effects of parameter uncertainties in design of linear control system
The first twelve system state variables are presented with the necessary mathematical developments f...
Progress reports on guidance and attitude control mechanisms of different flight vehicles are presen...
Data smoothing technique for parameter optimization in free flight orbit vehicle-borne tracking syst...
Least squares method for sequential guidance estimates on ballistic vehicle in partially known atmos...
Application of quadratic optimal control, least squares state, and parameter estimation to stability...
As a unified extension of a group of related mathematical procedures, Kalman filtering is of assista...
Thesis (Sc. D.)--Massachusetts Institute of Technology, Dept. of Aeronautical Engineering, 1967.Vita...
Control system optimization for Saturn 5 launch vehicles using gradient technique
This dissertation studies guidance and control of aerospace systems. Guidance algorithms are used to...
Research of control optimization, stochastic stability, and air traffic control problem
Research on flight control systems is reviewed. Investigations were conducted to evaluate and test a...
Least squares, minimum variance, and Kalman estimation applied to mathematical model of free flight ...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1998.Includes...
Integrated engine-airframe optimal control technology may significantly improve aircraft performance...
Design method including effects of parameter uncertainties in design of linear control system