Effect of Bearing Flexibility on Dual-Spin Satellite Attitude Stability

This publication has 5 references indexed in Scilit:

• Effects of flexibility in the bearing assemblies of dual-spin spacecraft
  AIAA Journal, 1971
• A set of r dynamical attitude equations for an arbitrary n-body satellite having r rotational degrees of freedom
  AIAA Journal, 1970
• The quadratic approximation in rotational dynamical equations
  Archive of Applied Mechanics, 1969
• Attitude stability criteria for dual spin spacecraft.
  Journal of Spacecraft and Rockets, 1967
• Stability analysis of mechanical systems with constraint damping.
  AIAA Journal, 1967