A motion control algorithm for microsatellite mock-up with flexible rods docking with
noncooperative target on the air table is proposed in the paper. A linear motion model of the …

The paper proposes a two‐stage algorithm for autonomous relative motion determination of
noncooperative and unknown object flying in space. The algorithm is based on image …

The angular motion of a CubeSat-type nanosatellite with a passive magnetic attitude control
system is mathematically modelled. The attitude control system consists of a permanent …

In this paper, a planar air-bearing test bed with unmanned aerial vehicles (UAV) was used to
test a microsatellite motion control system. The UAV mock-ups were controlled by four …

This paper considers the problem of determining the position of the center-of-mass and
inertia tensor of a microsatellite mockup on an air-bearing testbed by using optical …

The goal of the proposed 3U CubeSat mission is to test GNC system for a future flight to a
near Earth asteroid. In order to gain the goal a 3U CubeSat is to get to a vicinity of a space …

Abstract Space debris removal is one of the most important problems in space exploration.
This work is devoted to the development and testing of control algorithms for microsatellites …

The angular motion of a nanosatellite equipped with a hysteresis dam** system is studied.
The required number and sizes of hysteresis rods needed to achieve the specified transient …

Перед запуском космического аппарата (КА) все его системы проходят через ряд
лабораторных испытаний для подтверждения работоспособности. В частности …

Проводится математическое моделирование углового движения наноспутника типа
CubeSat с пассивной магнитной системой ориентации, в состав которой входят …