| 摘要 |
<p>Method involves definition of reference configurations such that a maneuver can be executed without singularities based on a reference configuration. Profiles are used to make a changeover from one reference configuration to another. If the current actuator configuration is not similar to a reference configuration, changeover to the reference configuration is made using a open loop profile. An Independent claim is made for a satellite with a system of gyroscopic actuators with a collection of reference configurations, whereby a maneuver can be generated without passing through a singularity by use of a reference configuration and with a set of profiles stored in the satellite enabling changeover from one reference configuration to another.</p> |
