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Algorithm for computing program values of angular velocity vector components during spacecraft terminal spatial turn in the inertial coordinate system
| Authors: Zubov N.E., Li E.K., Li M.V., Mikrin E.A., Poklad M.N., Ryabchenko V.N. | Published: 23.12.2015 |
| Published in issue: #6(105)/2015 | |
| DOI: 10.18698/0236-3933-2015-6-3-20 | |
| Category: Aviation, Rocket and Space Engineering | Chapter: Dynamics, Ballistics, Flying Vehicle Motion Control | |
| Keywords: kinematic equations, quaternions, boundary value problem, modal control, identification | |