Method for calculating spacecraft longitudinal motion parameters during landing on the surface of a small celestial body

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the legs operation peculiarities, changes of the horizontal and vertical
velocities of the spacecraft, and the spacecraft angular position after its
landing.
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The original manuscript was received by the editors on 22.05.2013
Contributors
Kazakovtsev V.P. — (Eng.), Professor of Engineering, Department of Dynamics and
Flight Control of Rockets and Spacecrafts, Bauman Moscow State Technical University,
author of over 120 research publications in the field of ballistics and flight dynamics of
spacecrafts and descent vehicles.
Bauman Moscow State Technical University, 2-ya Baumanskaya ul. 5, Moscow, 105005
Russian Federation.
34 ISSN 0236-3941. HERALD of the BMSTU. Series “Mechanical Engineering”. 2014. No. 1