This paper presents a new solar arrays deployment mechanism for space applications. It consists of a modular kinematic structure, which is operated by a single cable (1 DoF). Compared to traditional methods, this mechanism has the advantage of being reversible in the movement. Kinematic analysis of the mechanism is carried out in this work, as well as static analysis. They allow to define the main actuation parameters such as cable pull tension and spring stiffness. Moreover, suitable values for the mechanism parameters are computed by means of a dedicated algorithm
This work presents a novel spacecraft attitude control architecture using strain-actuated solar arra...
Tracking mechanisms were found to improve the performance of solar renewable energy systems that con...
Tracking mechanisms were found to improve the performance of solar renewable energy systems that con...
Abstract: Deployable structure technology has been used in aerospace and civil engineering structure...
With the advancement of membrane/blanket technology as an alternative choice to the conventional sol...
Solar array rotation mechanism provides a hinged joint between the solar panel and satellite body, s...
The paper investigates three critical areas in cable-driven rigid-panel solar arrays: First, the var...
Solar array rotation mechanism provides a hinged joint between the solar panel and satellite body, s...
In order to solve the problems of the existing solar wing, such as complex process and obvious struc...
In order to solve the problems of the existing solar wing, such as complex process and obvious struc...
As the International Space Station orbits around the earth, it goes through sunlight and the shadow ...
Solar array rotation mechanism provides a hinged joint between the solar panel and satellite body, s...
Flexible Printed Circuit Boards (Flex PCB) are commonly used for the electrical routing on spacecraf...
AbstractThis paper presents a novel hinge mechanism for deployment of spacecraft subsystems such as ...
This paper describes a Solar Array Deployment Mechanism (SADM) used to deploy a rigid solar array pa...
This work presents a novel spacecraft attitude control architecture using strain-actuated solar arra...
Tracking mechanisms were found to improve the performance of solar renewable energy systems that con...
Tracking mechanisms were found to improve the performance of solar renewable energy systems that con...
Abstract: Deployable structure technology has been used in aerospace and civil engineering structure...
With the advancement of membrane/blanket technology as an alternative choice to the conventional sol...
Solar array rotation mechanism provides a hinged joint between the solar panel and satellite body, s...
The paper investigates three critical areas in cable-driven rigid-panel solar arrays: First, the var...
Solar array rotation mechanism provides a hinged joint between the solar panel and satellite body, s...
In order to solve the problems of the existing solar wing, such as complex process and obvious struc...
In order to solve the problems of the existing solar wing, such as complex process and obvious struc...
As the International Space Station orbits around the earth, it goes through sunlight and the shadow ...
Solar array rotation mechanism provides a hinged joint between the solar panel and satellite body, s...
Flexible Printed Circuit Boards (Flex PCB) are commonly used for the electrical routing on spacecraf...
AbstractThis paper presents a novel hinge mechanism for deployment of spacecraft subsystems such as ...
This paper describes a Solar Array Deployment Mechanism (SADM) used to deploy a rigid solar array pa...
This work presents a novel spacecraft attitude control architecture using strain-actuated solar arra...
Tracking mechanisms were found to improve the performance of solar renewable energy systems that con...
Tracking mechanisms were found to improve the performance of solar renewable energy systems that con...