Ground simulation of spacecraft motion simulating all six degrees of freedom is a challenging problem due to several features of the natural dynamics in space that are difficult to reproduce on ground. Unlike terrestrial (aerial, land or underwater) vehicles, space vehicles have an overwhelmingly large percentage of their total energy in their translational motion. Dynamical coupling between the translational and rota-tional degrees of freedom can significantly affect the attitude motion of spacecraft. The attitude motion is particularly important for a spacecraft tasked to autonomously ren-dezvous and capture or dock with a target object in space. Here we present a ground simulator design for 6 DOF simulation of spacecraft engaged in auton...
Ground testing of multi-spacecraft proximity operations with hardware in-the-loop is currently an ex...
The design of most hardware-based spacecraft attitude simulators restricts motion in one or more axe...
Orbital robotics, due to the unfriendly environment (radiation, micro-gravity, thermal stresses, etc...
The successful prediction of spacecraft motion is often heavily based upon assumptions used to simpl...
A novel testbed is introduced to examine the problem of multiple spacecraft interacting in close pro...
This paper presents a method to control a manipulator system grasping a rigid-body payload so that t...
In this paper we present the concept design and the progress in the realization of a spacecraft mot...
Future logistics supply and servicing vehicles such as cargo transfer vehicles (CTV) must have full ...
In this paper we describe a new experimental facility at the School of Aerospace En-gineering at Geo...
This paper presents a new six-degree-of-freedom robotic spacecraft simulator, the Multi-Spacecraft T...
A spacecraft formation possesses several benefits over a single-satellite mission. How-ever, launchi...
Increasing access to space has driven demand for low cost, portable, and highly specialized robotic ...
This thesis developed a 3-DOF satellite simulator with an attached 3-DOF manipulator to capture and ...
The article of record as published may be found at https://dx.doi.org/10.1016/j.paerosci.2019.100552...
Abstract—We are developing an autonomous mo-bile robotic system to emulate six degree of freedom rel...
Ground testing of multi-spacecraft proximity operations with hardware in-the-loop is currently an ex...
The design of most hardware-based spacecraft attitude simulators restricts motion in one or more axe...
Orbital robotics, due to the unfriendly environment (radiation, micro-gravity, thermal stresses, etc...
The successful prediction of spacecraft motion is often heavily based upon assumptions used to simpl...
A novel testbed is introduced to examine the problem of multiple spacecraft interacting in close pro...
This paper presents a method to control a manipulator system grasping a rigid-body payload so that t...
In this paper we present the concept design and the progress in the realization of a spacecraft mot...
Future logistics supply and servicing vehicles such as cargo transfer vehicles (CTV) must have full ...
In this paper we describe a new experimental facility at the School of Aerospace En-gineering at Geo...
This paper presents a new six-degree-of-freedom robotic spacecraft simulator, the Multi-Spacecraft T...
A spacecraft formation possesses several benefits over a single-satellite mission. How-ever, launchi...
Increasing access to space has driven demand for low cost, portable, and highly specialized robotic ...
This thesis developed a 3-DOF satellite simulator with an attached 3-DOF manipulator to capture and ...
The article of record as published may be found at https://dx.doi.org/10.1016/j.paerosci.2019.100552...
Abstract—We are developing an autonomous mo-bile robotic system to emulate six degree of freedom rel...
Ground testing of multi-spacecraft proximity operations with hardware in-the-loop is currently an ex...
The design of most hardware-based spacecraft attitude simulators restricts motion in one or more axe...
Orbital robotics, due to the unfriendly environment (radiation, micro-gravity, thermal stresses, etc...