INERTIAL GUIDANCE, ITS EVOLUTION AND FUTURE POTENTIAL
Space science - navigation - inertial guidance
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Space science - navigation - inertial guidance
Space science - launch vehicle and carrier rocket guidance-control systems
This paper contains progress reports of NASA-sponsored studies in the areas of space flight theory and guidance theory. The studies are carried on by several universities and industrial companies. This progress report covers the period from June 15, 1962 to December 20, 1962. The technical supervisor of the contracts is W.E. Miner, Deputy Chief of the Future Projects Branch of Aeroballistics Division, George C. Marshall Space Flight Center.
Spacecraft guidance - numerical integration - computer method
Perturbation control for midcourse guidance in space trajectory program
Guidance sensor for high precision control of oao needed when examining radiation from selected stars
Guidance systems and flight optimization theory for space flight
Numerical analysis of adaptive control systems - guidance systems
Linear programming for approximate computation of guidance function for adaptive control systems
Minimum fuel vertical touchdown lunar landing guidance technique
Guidance policies for multiple-impulse correction of spacecraft trajectory
Nonlinear guidance system for descent trajectories
Interrupted-braking guidance system for soft lunar landings
Optimization of space-vehicle trajectories by use of iterative guidance mode that minimizes midflight recalculation time for new optimum trajectories
Calculus of variation methods used for trajectory optimization and guidance of rocket propelled vehicles
Problems involved in meeting trajectory and guidance requirements for the return-to-earth and atmospheric reentry of a lunar spacecraft
Motion equations - iterative guidance scheme for ascent to orbit
Nasa research in space flight and guidance theory