NASA Technical Reports Server (NTRS) 19810009554: Equilibrium and stability of a satellite influenced by gravitational and aerodynamic torquesReport as inadecuate



 NASA Technical Reports Server (NTRS) 19810009554: Equilibrium and stability of a satellite influenced by gravitational and aerodynamic torques


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A circular orbit and constant atmospheric density was assumed. A computer program which determines equilibrium attitudes and the associated eigenvalues of these attitudes is presented. Demonstration of the use of this program was made using the former Skylab satellite as an example.


Author: NASA Technical Reports Server (NTRS)

Source: https://archive.org/







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