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Volume 17 Number | 1 |
Optimal Attitude Control in the Reorientation of a SatelliteGyrostat S I Zlochevskii | 13 |
Ballistic and Navigation Aspects of the Braking Problem for a Spacecraft in Jupiters | 25 |
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according allowance altitude analysis angle approximation assumed atmosphere axis body boundary burst calculated carried characteristics close cloud coefficient component computed connected consider constant coordinates correction corresponding curves density dependence descent determined direction distance distribution earth effect electron elements energy entry equal equations errors estimate experiment field flares flight flux function given height increase indicated initial integral intensity layer limit magnetic mass maximum mean measurements method Moscow motion observed obtained orbit Original parameters particles period phase plane position possible present problem radiation radio range recorded region relation relative respect rotation Russian satellite scattering shown shows solar solution space spacecraft spectra spectrum structure surface Table temperature tion trajectory values variation vector velocity Venera 11 Venus wave wind