Slew guidance method for spacecraft
View Patent ↗A method is adapted for slewing a body from an initial state to merge with a desired state profile. In an embodiment, the method includes the steps of (a) obtaining data indicative of a time profile of desired future states for the body; (b) searching sequentially through the time profile of desired future states; (c) calculating several slews for the body from the initial state to each of the desired future states; (d) determining the earliest future state to which the body can actually slew; (e) choosing the minimum-energy slew to that state; and (f) causing the body to perform that chosen slew.
1. A method for slewing a body from an initial state to merge with a desired state profile, comprising:
obtaining data indicative of a time profile of desired future states for the body;
searching sequentially through the time profile of desired future states;
calculating a slew for the body from the initial state to each of the desired future states;
calculating an initial future time;
determining whether the body can slew to the desired state profile within a sufficient amount of time such that the desired state profile can be achieved by the initial future time;
if the body cannot slew to the desired state profile within a sufficient amount of time such that the desired state profile can be achieved by the initial future time, then recalculating a new slew for the body that will achieve the desired state profile by the initial future time; and
causing the body to slew pursuant to the newly calculated slew.
2. A method as in claim 1 , wherein the body is a spacecraft.
3. A method as in claim 1 , wherein the state profile includes angular attitude and angular rates.
4. A method as in claim 1 , wherein data indicative of a time profile of desired future states is uploaded from a spacecraft or a ground station.
5. A method as in claim 1 , wherein data indicative of a time profile of desired future states resides in a local memory.
6. A method as in claim 1 , wherein a state profile includes 2-axis attitudes and rates.
7. A method as in claim 1 , wherein a state profile includes fully constrained 3-axis attitudes and rates.
8. A method as in claim 1 , wherein there is a secondary parameter to be optimized after slew duration.
9. A method as in claim 8 , wherein the secondary parameter to be optimized after slew duration comprises slew actuation energy to be minimized.