Abstract
Although the small stature of CubeSats and their standardized deployer options help to lower unit development cost and facilitate launch opportunities, the physical size limits of CubeSats prove to be a double-edged sword vis-à-vis sustaining a stable power state while hosting instruments with high power demands and often strict pointing requirements. For the Space Weather Atmospheric Reconfigurable Multiscale-EXperiment (SWARM-EX), this issue is magnified by the mission’s ambitious goals; to comply with mission requirements, a SWARM-EX spacecraft is required to concurrently (1) point the science instruments no more than 30° off ram when they are operational, (2) point the GPS patch antenna no more than 30° off zenith at least once per orbit, (3) point the boresight of the X-Band patch antenna no more than 18° from the ground station during downlink, (4) maximize the differential cross-sectional area during differential drag maneuvers, and (5) maximize solar array power generation at all times. Consequently, leading-edge CubeSat missions like SWARM-EX require innovative systems engineering solutions to remain power-positive during on-orbit operations. Through the design of a comprehensive module-based concept of operations, orbital power generation simulations, intricate constrained attitude profiles, and a configurable battery state of charge simulation tool, the SWARM-EX mission designers have conceived a plan to retire the risk of not maintaining a power-positive state while successfully meeting all mission requirements; it is the aim of the authors to illuminate these strategies as a case study.
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