Research Article
Time-Optimal Attitude Scheduling of a Spacecraft Equipped with Reaction Wheels
Figure 9
Attitude parameters of a minimum-time rest-to-rest maneuver of the spacecraft between the target attitudes and given in Table 1. The solution obtained with the fifth-degree Gauss-Lobatto direct collocation method is represented with continuous lines whereas the solution obtained with the pseudospectral method is represented with dashed lines.