Affiliation:
1. Massachusetts Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Reference11 articles.
1. Spacecraft Attitude Determination and Control
2. 4Weick, F. E. “Propeller Design, Practical Application of the Blade Element Theory - I,” Tech. Rep. TR235, National Advisory Committee for Aeronautics, 1926.
3. NPSNET: Flight Simulation Dynamic Modeling Using Quaternions
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