公开(公告)号：US20220169404A1

公开(公告)日：2022-06-02

申请号：US17434617

申请日：2020-02-28

Applicant: OQAB DIETRICH INDUCTION INC.

Inventor： Haroon B. Oqab ,  George B. Dietrich

IPC: B64G1/24 ,  B64G1/62 ,  B64G1/64 ,  B64G4/00 ,  B64G1/10

Abstract: An example system for controlling a target satellite includes: a satellite-control spacecraft including: a propulsion subsystem configured to propel and navigate the spacecraft proximate the target satellite; and a satellite-capture subsystem configured to: capture the target satellite; apply a control medium to the target satellite, the control medium including an electrically conducting and/or magnetic material; and release the target satellite; and an energization assembly configured to energize the control medium to release energy for controlling, propelling and navigating the target satellite.