This investigation analyzed the influence of design variables (L, y, t, and x) of a new flexible
hinge displacement amplification mechanism on (i) magnification ratio,(ii) maximum …

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 …

A non-contact vibration measurement and control system for a piezoelectric-patched flexible
cantilever plate is presented, using laser displacement sensors. Two laser displacement …

Methods for dynamic parameters identification and vibrations estimation of large spacecraft
with flexible structures are reviewed. Different approaches to the structural deviation …

To more accurately characterize the deformation behavior of flexible links during rotation,
the two-dimensional (2D) deformation and friction torque are considered at the same time …

The methods of stabilization of a spacecraft (SC) main body with two flexible elements
(antenna and panel) are studied in this paper. The process of stabilization is impeded by …

This paper proposes a distributed vibration control strategy based on reinforcement learning
to solve the vibration control problem of large flexible satellite solar panel. The main …

Attitude control of a satellite with three flexible elements is considered. Control torque is
developed by a set of reaction wheels, which are installed on the central hub of the satellite …

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 …

Изучаются методы стабилизации корпуса космического аппарата с двумя нежесткими
элементами–антенной и панелью. Процессу стабилизации корпуса препятствуют …