Orbit optimization and laser applications, Issues 92-93
North Atlantic Treaty Organization, Advisory Group for Aerospace Research and Development - Science - 484 pages
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The Application of Dynamic Programming to Orbit Transfer
ORBIT TRANSFER PROCESSES AS DISCRETE DECISION PROCESSES
31 other sections not shown
acceleration accelerometer alii amplifier angle angular Applied approximately attitude axis bandwidth bending mode birefringent boundary coefficients components control system coordinate system cutoff demodulation detection detector determined differential equation digital computer dynamic programming earth effects Electronic engine filter flight frequency translation function gimbal gravitational guidance computer guidance equations guidance scheme guidance system heterodyne inertial measuring unit initial conditions injection input integrating laser launch vehicle linear loop Lunar Excursion Module mass matrix maximum principle methods microwave minimize mission navigation and guidance noise obtained operation optimal orbit transfer orbit transfer process orbital parameters oscillator output performance index perturbations phase photodetector photomixer photomultiplier polynomial position and velocity problem propulsion pumping radiation range rate gyro ratio rendezvous rendezvous problem S-IVB satellite shot noise shown in Figure signal simulation solar solution space chambers space vehicle spacecraft spectral stabilization stage surface techniques temperature terminal errors thermal thrust thrust vector values variables