Nonlinear feedback solution for minimum-time injection into circular orbit with constant thrust acceleration magnitude
Nonlinear feedback solution for minimum-time injection into circular orbit with constant thrust acceleration magnitude
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Nonlinear feedback solution for minimum-time injection into circular orbit with constant thrust acceleration magnitude
Stiffener eccentricity and location influence on minimum weight design aspects of stiffened cylinders under compression
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Minimum energy reaction wheel control for Advanced Orbiting Solar Observatory performing raster scan over small celestial area
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Charge and energy spectrum of heavy nuclei during solar minimum, 1965
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Uniqueness of extremal controls for minimum fuel problems pertaining to single input linear time- invariant systems
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Analytic solution obtained for minimum impulse transfer between two neighboring low eccentricity orbits