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Algorithms for Radio Guidance with Application to Control of Landing of Spacecraft | 33 |
Optimal Correction of the Guidance Trajectory of a Spacecraft IIV V Malyshev | 43 |
The Problem of Continuous Earth Coverage and Kinematically Regular Satellite Networks II | 52 |
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according activity altitude analysis angle angular approximately assume atmosphere axis boundary calculated characteristic coefficients component concentration considered constant coordinates correction corresponding cosmic rays curves density dependence derivatives determined direction distribution drift earth effect electron elements energy equal equations error estimates experiment expression Figure flight flux function geomagnetic given height increase indicated initial integral intensity interval ionosphere latitudes limit magnetic field mass matrix maximum mean measurements method motion observed obtained operation orbit parameters particles period phase plane polar position possible presented probe problem protons publisher radiation range recorded region relations relative respect Russian satellite shown shows side solar solution space spacecraft spectrum surface Table taken temperature tion trajectory values variations vector vehicle velocity