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Choice of Ballistic Characteristics and Control Method for a Lifting Spacecraft Designed | 35 |
Optimal Control during Descent to the Surface of an Atmosphereless Planet | 44 |
Rotational Motion of an Astronauts Trunk Ya M Shapiro | 51 |
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according altitude angle angular approximation assume atmosphere average axis boundary calculated characteristic coefficient components concentration considered constant coordinates corresponding curve decrease density dependence described determined direction distribution earth effect electrons energy equal equations error estimate experiment expression factor field flares flux frequency function Geophys given height increase indicated initial intensity interval ionospheric Issled Kosm latitudes layer limits magnetic Mars mass maximum means measurements mechanical method motion observed obtained occurs optimal orbit Original parameters particles period phase plane plasma polar position possible present problem protons publisher quantity radiation range recorded region relations relative respect rotation Russian satellite shown shows solar solution space spacecraft spectrum stability surface Table temperature tion trajectory values variations vector velocity wave