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Algorithm for the Determination of the Optimal ThreeImpulse Transition | 1 |
Motion of a Symmetrical Satellite About Its Center of Mass in a Circular | 10 |
Rejection of Anomalous Observations in Determining the Trajectories | 16 |
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according altitude analysis angle approximation assume atmosphere average axis body boundary calculated carried characteristic coefficients components concentration consider coordinate corresponding curves density dependence determined diffusion direction distance distribution earth effect electric field electrons elements energy engines equal equations errors estimate example experiment experimental expression flux function Geophys given increase indicated initial integral intensity ionosphere issues latitude layer limits magnetic field magnetosphere mass maximum means measurements method Moscow motion observed obtained optimal orbit orientation parameters particles period perturbations plane plasma polar position possible presented problem processes protons radiation range region relations relative respect rotation Russian satellite shown solar solution space spacecraft spectra spectrum stability surface Table tion trajectory transfer values variables variations vector velocity Venus