Guidance and control technology for manned planetary missions.
Manned spacecraft guidance and control technology from Mercury, Gemini and Apollo programs, including hardware, software, man machine systems, etc
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Manned spacecraft guidance and control technology from Mercury, Gemini and Apollo programs, including hardware, software, man machine systems, etc
Fine guidance sensor for OAO, detailing sample and hold circuit design to solve error problems from electro-optical elements
Manual optimal guidance schemes for space vehicles to minimize computational and display requirements for pilot task loading
Spacecraft optical guidance, navigation and control instrumentation selection criteria for manned space missions, discussing space flight observable data role
Equations implementing closed loop control in explicit guidance systems
Apollo gyro reliability covering guidance, navigation and control systems, stressing failure mode prediction
Navigation and guidance of two stage hypersonic/ rocket spacecraft launch vehicle for rendezvous mission
Evaluation method for strapdown spacecraft guidance systems on automated interplanetary missions, using cost and system performance efficiency probability model
Statistical methods for alignment processing of strapdown inertial guidance systems
Atlas/Centaur/Surveyor flights guidance accuracy, discussing postflight analysis of injection errors due to hardware, software and propulsion system
Low thrust station keeping guidance scheme for gravity gradient stabilized 24-hour satellite, solving equations of motion for near circular equatorial orbit
Adaptive guidance scheme for minimum fuel two finite burns rendezvous from elliptical parking orbit to coplanar circular orbit
Spacecraft guidance analysis of mulitiple outer planet mission utilizing gravity assist swingbys to achieve planetary flybys with single spacecraft
Onboard guidance and control computers, discussing component technology for long term deep space missions
Manual optimal guidance scheme using predictive display applied to launch vehicles during boost for continuous generation of predicted fuel- optimal trajectory
Optimal stochastic midcourse guidance, analyzing correction programs employing feedback gain matrix
Planetary and deep space mission guidance and control technology requirements
Onboard computer equations for rocket vehicle guidance to elliptical orbit, discussing iteration absence from computations and digital simulation results