where and are control inputs ("drive" and
"steer"). The linearization at the origin is obviously not completely controllable (check this!)
By computing and , show that the nonlinear
system is completely controllable.
2. Show that the system from Problem 1 fails Brockett's condition, i.e., the origin is not
- stabilizable.
3. Consider the model of a spacecraft with thrusters generating torque around two axes:
where is the angular velocity,
is the attitude (in modified Rodrigues parameters),
are the torque inputs,
the matrix is a skew-symmetric matrix defined as
and the matrix is defined as
.
The linearization at the origin is obviously not completely controllable (check!).
By computing , and , show that the nonlinear
system is completely controllable whenever .
4. Show that the system from Problem 3 fails Brockett's condition. Note that