B021-0002
GEDI Precision Attitude Determination
Abstract:
GEDI PAD, along with real-time pointing control, are accomplished with 3 DTU Star Tracker heads. Each head comes with an integrated MEMS micro inertial reference unit (MIRU). Due to a restricted field of view, as well as the harsh glinting and blockage environment on the ISS, all trackers are often blinded and present challenges to achieving an optimal PAD solution. The ground post-processed PAD implements a Multiplicative Extended Kalman Filter (MEKF) and Rauch-Tung-Striebel (RTS) filter. The filter states include attitude corrections to the attitude reference frame, angular rate biases, and relative alignment estimates to each tracker. The GEDI mission’s challenging geolocation budget requires attitude solutions to be better than 4.5 arcseconds 1σ, with an overall geolocation knowledge budget of 10 m. Of particular note is the novel use of ISS attitude data to constrain the GEDI PAD solutions during significant GEDI tracker blinding and poor performance periods. We present the performance of the PAD solutions during ideal data collection, and also during significant blinding and glinting periods. We discuss the current PAD performance and its impact on the overall precise geolocation error budget, as well as future improvements and expected performance.