Kinematic variables in the equations of motion of a rigid body in the atmosphere

Details Kinematic variables in the equations of motion of a rigid body in the atmosphere Kinematic variables in the equations of motion of a rigid body in the atmosphere

Jan 1988

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1988kosis..26..157l&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 26, Jan.-Feb. 1988, p. 157-159. In Russian.

Physics

Astrodynamics, Atmospheric Entry, Equations Of Motion, Reentry Physics, Kinematic Equations, Quaternions, Satellite Orientation

Scientific paper

Three systems of kinematic variables are compared for a model problem involving regular precession and for an actual problem involving spacecraft descent in the atmosphere. A fourth-order Runge-Kutta method was used for the numerical integration of the kinematic and dynamic equations of motion. The use of a quaternion approach to solving the equations of motion of a rigid body in the atmosphere is recommended.

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