FULL-LENGTH PAPERS - Epicyclic Motion of Satellites Under Rotating Potential
AIAA-2004-5339 A Simple High Accuracy Inetgrator for Spacecraft Attitude Systems
Autonomous On-Board Batch Filter for Near Circular Orbit Determination
In-orbit Attitude and Orbit Control Commissioning of UoSAT-12
Full Attitude from a Single GPS Antenna: Demonstration of Concept with Orbital Data from PoSAT-1
NigeriaSat-2 AOCS: Results from the First 90 Days in Orbit (AAS 12-093)