FINE GUIDANCE SENSOR FOR HIGH PRECISION CONTROL OF THE OAO
Fine guidance sensor of the cassegrain telescope of the orbiting astronomical observatory /oao/
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Fine guidance sensor of the cassegrain telescope of the orbiting astronomical observatory /oao/
Presentation of means for achieving statistically optimal measurement and/or feedback gain programs for midcourse guidance
Nonlinear terminal guidance system for descent trajectories including soft landing
Modified proportional navigation guidance /mpn/ technique allows simplified, automatic, pinpoint lunar landing with minimum fuel expenditure
Earth-based radio command of midcourse guidance for lunar flights is described, noting spacecraft, tracking station, and computing facility requirements
Atmospheric reentry guidance and control methods - bibliography
Current status of navigation, guidance, and control
Unified lunar spacecraft guidance of major and minor maneuvers during accelerated and coasting flight
Navigation and guidance problems involving flight path calculations and spacecraft state vector evaluation, using Mars midcourse navigation as example
Guidance and navigation equipment used by both Apollo service module and lunar excursion module
Guidance system for accurate soft lunar landing including error sensitivities evaluation and applications to Saturn V Lunar Logistic Vehicle
Onboard optical guidance system for planet-bound spacecraft including covariance matrices for orbital parameters, system and instrument biases and parametric course accuracy curves
Minimum effort theory for interplanetary spacecraft guidance and control
Earth-based midcourse guidance for Mariner Mars 1964 space probe, using small rocket engine to obtain desired trajectory correction
Midcourse navigation, guidance, and control simulation techniques for manned spacecraft
Sensor requirements for spaceborne navigation, guidance, and control system for unmanned lunar landing vehicle
Linear guidance equations for impulse velocity corrections in space missions
Gyroscopic drift and Markov process research in inertial guidance system components study