CPC B64G 1/242 (2013.01) [B64G 1/244 (2019.05); B64G 2001/247 (2013.01)] | 15 Claims |
1. A method comprising:
determining, by use of a processor, a power collection function for a satellite;
determining a power cost function Cαw for the satellite as Cαw=Σt0tfp(t)dt wherein p(t) is a reaction wheel consumption for time t the satellite slews from a first frame t0 to a second frame t;
determining a cost function Ji(xN) from the power collection function and the power cost function as Ji(xN)=−CpPbN+Cθ(x2N−θd)2 wherein PbN is battery charge, Cp is a nonzero weighting factor for the battery charge, Cθ is power collected, x is a satellite position, and θd is a satellite orientation;
calculating a power enhanced slew maneuver by minimizing the cost function subject to the power collection function and the power cost function; and
maneuvering the satellite with the power enhanced slew maneuver.
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