Minimum fuel attitude control of a nonlinear satellite system with bounded control by a method based on linear programming
Optimal control method based on linear programming for satellite fuel consumption
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Optimal control method based on linear programming for satellite fuel consumption
Measurement and display studies of information for remote manipulation and manual control
Earth reflected solar radiation and stability of satellite thermal control coatings, noting intensity distribution shifting toward UV region and coatings degradation rate
Wind tunnel evaluation of Apache model aerodynamic stability and control characteristics
Design and tests of Lunar Orbiter guidance and control systems
Stabilization and control systems for reentry vehicle
Neighboring optimal feedback control of multi-input nonlinear dynamic systems
Computerized performance evaluation of Apollo thrust vector digital autopilot control system
Twin gyro coupling system with compensation and nonlinear control for satellite attitude stabilization
Mechanical and nonmechanical controls for earth and space storable propellants for liquid rocket propulsion
This design survey summarizes the history of the Orbiting Geophysical Observatories' (OGO) Attitude Control Subsystem (ACS) from the proposal phase through current flight experience. Problems encountered in design, fabrication, test, and on orbit are discussed. It is hoped that the experiences of the OGO program related here will aid future designers.
Control theory, Volume 1, covering linear, nonlinear, stochastic, optimal, adaptive and learning systems, sensitivity analysis, etc
Optimal control surface location for flexible aircraft determined by matrix minimum principle and calculus of variations
Integrated temperature and humidity control and water recovery subsystem for manned test in space station simulator
Inventory control of mercury condensing pressure during SNAP 8 startup
Deadband condenser inlet pressure control method for SNAP 8 startup
Control algorithm for optimization of nonlinear stochastic processes with discounted performance criteria
Systems design criteria for spacecraft attitude control during thrusting maneuvers