Abstract
The paper adopts the energy shaping method to control of rotational motion. A global representation of the rigid body motion is given in the canonical form by a quaternion and its conjugate momenta. A general method for motion control on a cotangent bundle to the 3-sphere is suggested. The design algorithm is validated for three-axis spacecraft attitude control
| Original language | Danish |
|---|---|
| Publication status | Published - 2001 |