The VISION – Concept of laser crosslink systems using nanosatellites in formation flying
Spacecraft fuel-optimal and balancing maneuvers for a class of formation reconfiguration problems
Spacecraft formation flying system design and controls for four nanosats mission
Hybrid optimization for multiple-impulse reconfiguration trajectories of satellite formation flying
Hardware-in-the-loop simulations of GPS-based navigation and control for satellite formation flying
Analytical solution to optimal relocation of satellite formation flying in arbitrary elliptic orbits