Abstract
This paper proposes a description of flexible spacecrafts’ motion and rotation uniformly with dual quaternions. The dynamic equations are derived by using Lagrange equations. Recursive Newton-Euler (RNE) method is introduced to calculate the nonlinear terms in the equations. The simulation results demonstrate the coupling effects during the actuating speed switch of the solar panel.
Full Text 
Sign-in/Register to access full text options
Sign-in/Register to access full text options 
Published version (
Free)
Free) 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a call
