Add to ORKGThesis (Sc. D.)--Massachusetts Institute of Technology, Dept. of Aeronautical Engineering, 1967.Vita.Includes bibliographical references (leaves 155-160).by John Jacob Deyst, Jr.Sc.D
Optimal control theory has been successfully applied to a wide range of a problems in spacecraft tra...
Linear optimal control techniques used as synthesis tool to conceptually design control systems for ...
Two problems are presented in the area of optimal control and its application to the design of attit...
Time and fuel optimal control problems associated with controlling spacecraft under noisy measuremen...
This dissertation studies the influence of uncertainty on spacecraft control. The sources of the un...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991.In...
Research of control optimization, stochastic stability, and air traffic control problem
The research carried out in the areas of optimal control and estimation theory and its applications ...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1994.In...
Mathematical analyses of suboptimal attitude maneuvering control for synchronous earth pointing sate...
Numerical solution of stochastic Hamilton-Jacobi equation for fuel optimal spacecraft attitude contr...
Computationally useful algorithms are considered that can aid the control engineer in designing syst...
Re-entry trajectory design problem of a space capsule into the Martian atmosphere is investigated wi...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991.Ti...
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1971. Sc.D.Mic...
Optimal control theory has been successfully applied to a wide range of a problems in spacecraft tra...
Linear optimal control techniques used as synthesis tool to conceptually design control systems for ...
Two problems are presented in the area of optimal control and its application to the design of attit...
Time and fuel optimal control problems associated with controlling spacecraft under noisy measuremen...
This dissertation studies the influence of uncertainty on spacecraft control. The sources of the un...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991.In...
Research of control optimization, stochastic stability, and air traffic control problem
The research carried out in the areas of optimal control and estimation theory and its applications ...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1994.In...
Mathematical analyses of suboptimal attitude maneuvering control for synchronous earth pointing sate...
Numerical solution of stochastic Hamilton-Jacobi equation for fuel optimal spacecraft attitude contr...
Computationally useful algorithms are considered that can aid the control engineer in designing syst...
Re-entry trajectory design problem of a space capsule into the Martian atmosphere is investigated wi...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991.Ti...
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1971. Sc.D.Mic...
Optimal control theory has been successfully applied to a wide range of a problems in spacecraft tra...
Linear optimal control techniques used as synthesis tool to conceptually design control systems for ...
Two problems are presented in the area of optimal control and its application to the design of attit...