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Fundamentals of Spacecraft Attitude Determination and Control
part of the Space Technology Library series
- Binding:
- Hardback
- Pages:
- 486
- Published:
- May 31, 2014
- Edition:
- 2014
- Dimensions:
- 245x167x33 mm.
- Weight:
- 898 g.
Delivery:
2-3 weeks
Expected delivery: December 14, 2024
Description of Fundamentals of Spacecraft Attitude Determination and Control
It provides detailed derivations for attitude kinematics and dynamics and provides detailed description of the most widely used attitude parameterization, the quaternion.
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