Three-point peaking with Kalman filtering improves satellite antenna alignment under signal noise while reducing drive wear and motion requests.
A bounded range-range grid finds all candidate orbits from angle-only measurements, then refines and clusters them with covariance estimates.
Projection-based screening removes high-error observation points in space station common-view time comparison, cutting orbit error impact below 300 ps.
Imaging-guided LIDAR tracking captures angular position and range of small resident space objects beyond ground-based limits.