A linear algorithm for determining relative orbital state using angle data
Linear algorithms for determining spacecraft relative orbital state using angle data with digital computer
Schneider, A. M.↗
Engineering topics
Publications and source records attributed to Schneider, A. M..
Linear algorithms for determining spacecraft relative orbital state using angle data with digital computer
Moderately elliptic reference orbit perturbed motion, applying linearized perturbation equations for circular orbit
Manual spacecraft rendezvous system based on handheld instruments and manual computations, considering error analysis and simulation
Spacecraft navigation, guidance and control for manual rendezvous with orbiting target, examining error sources perturbing effects
Automatic control systems for electron bombardment and contact ion engines
Cesium vapor automatic control systems for electron bombardment and contact ion engines