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Determining the Orientation of an Artificial Satellite in a TwoVector | 1 |
Volume 16 Number | 3 |
Volume 16 Number | 4 |
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according altitude angle angular approximation assumed atmosphere average axes axis body boundary calculated characteristic coefficient components concentration consider constant coordinates corresponding curve decrease density dependence determined direction distance distribution earth effect electron energy equal equations error estimate experimental experiments expression field flare flight flux frequency function given height increase indicated integral intensity interval ionosphere Issled Kosm layer limits magnetic field magnetosphere Mars matrix maximum mean measurements method motion observed obtained optimal orbit parameters particles planet plasma position possible present problem protons radiation radio range ratio recorded region relation relative respect Russian satellite scattering shown shows side singular solar wind solution space spacecraft spectral spectrum stability surface Table temperature tion trajectory transfer values variations vector vehicle velocity Venera Venus wave zone