Electronic Resource
Springer
Celestial mechanics and dynamical astronomy
9 (1974), S. 21-39
ISSN:
1572-9478
Source:
Springer Online Journal Archives 1860-2000
Topics:
Physics
Notes:
Abstract The implications of flexible appendages on the attitude dynamics of a space vehicle are examined in general terms. Two families of natural vibration modes, referred to as ‘constrained’ and ‘unconstrained’, are discussed and the relationships between them derived. The incorporation of either set of modes into a simulation of the general attitude motion (under the influence of perturbing torques and control torques) is explained. The influence of rotors on these results is also explored.
Type of Medium:
Electronic Resource
URL:
http://dx.doi.org/10.1007/BF01236162
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