For the near-distance rendezvous problem of spacecraft, the classical guidance methods,
such as R-bar and V-bar, are restricted by the initial relative positions and velocities and …

Optimization-based control has undoubtedly gained an enormous amount of both interest
and considerable success in the aerospace industry. Many effective tools have been …

Differential Seeded Secant (SDSS) numerical iteration method for computing the semi major
axis of a perturbed orbit based on the anomalistic period is presented. Specifically, the value …

On-orbit satellite servicing is critical to maximizing space utilization and sustainability and is
of growing interest for commercial, civil, and defense applications. Reliance on astronauts or …

This investigation deals with the problem of spacecraft relative motion control, which is
typically associated with the spacecraft rendezvous and proximity maneuvers. Relative …

In this paper, a novel-filtering algorithm for the relative orbit determination of non-
cooperative maneuvering target is proposed. The algorithm is based on the Strong Tracking …