Analytical solution of a gravity gradient axisymmetric satellite in eccentric orbits

1989 ◽  
Vol 50 (6) ◽  
pp. 2187-2203 ◽  
Author(s):  
A. C. SOUDACK ◽  
V. J. MODI ◽  
A. C. NG
2012 ◽  
Vol 2012 ◽  
pp. 1-15 ◽  
Author(s):  
Juan F. San-Juan ◽  
Luis M. López ◽  
Rosario López

A higher-order perturbation theory for the rotation of a uniaxial satellite under gravity-gradient torque demonstrates that known special configurations of the attitude dynamics at which the satellite rotates, on average, as in a torque-free state, are only the result of an early truncation of the secular frequencies of motion. In addition to providing a deeper insight into the dynamics, the higher order of the analytical solution makes it competitive when compared with the long-term numerical integration of the equations of motion.


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