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Analysis of the impact of implementation methods of three-parameter approach to modeling the angular dynamics of movement of the aircraft
Authors: Lysikova V.S. | Published: 04.12.2018 |
Published in issue: #11(28)/2018 | |
DOI: DOI: 10.18698/2541-8009-2018-11-410 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
Keywords: aircraft dynamics, coordinate systems, Euler angles, direction cosine matrix, transition schemes between starting and associated coordinate systems, angular motion of the aircraft, three-parameter approach to modeling, mathematical description of the flight |