Add to ORKGA prototype docking mechanism for the Space Station was designed and fabricated for NASA. This docking mechanism is actively controlled and uses a set of electromechanical actuators for alignment and load attenuation. Dynamic tests are planned using the Marshall Space Flight Center's 6-DOF Motion Simulator. The proposed tests call for basic functionality verification as well as complete hardware-in-the-loop docking dynamics simulations
Proposed future space exploration, such as lunar and Martian expeditions, will require autonomous do...
The primary purpose of the OMV is to dock with orbiting payloads and then either transfer them to a ...
The soft capture system of the NASA Docking System (NDS) is a mechanism with six-degrees of freedom ...
The Space Station/Space Operations Mechanism Test Bed consists of the following: a hydraulically dri...
TRW has conducted an extensive Contact Dynamics Test Program (CDTP) of the Three Point Docking Mecha...
Europe's first confrontation with docking in space will require extensive testing to verify design a...
Extensive dynamic testing was conducted to verify the flight readiness of the Apollo docking hardwar...
One of the most critical operational functions for the space station is the orbital docking between ...
The Space Station Mechanism Test Bed consists of a hydraulically driven, computer controlled six deg...
In this paper, an analytical approach for studying the contact dynamics of space-based vehicles duri...
This paper discloses the design procedure of a docking mechanism for space applications. The mechani...
Logicon Control Dynamics develops contact dynamics models for space-based docking and berthing vehic...
The objective of the STRONG mission is the deployment of payloads from Low Earth Orbit into greater ...
This presentation describes the application of robotic and computer vision systems to validate docki...
Design and fabricate test hardware for NASA's George C. Marshall Space Flight Center (MSFC) are repo...
Proposed future space exploration, such as lunar and Martian expeditions, will require autonomous do...
The primary purpose of the OMV is to dock with orbiting payloads and then either transfer them to a ...
The soft capture system of the NASA Docking System (NDS) is a mechanism with six-degrees of freedom ...
The Space Station/Space Operations Mechanism Test Bed consists of the following: a hydraulically dri...
TRW has conducted an extensive Contact Dynamics Test Program (CDTP) of the Three Point Docking Mecha...
Europe's first confrontation with docking in space will require extensive testing to verify design a...
Extensive dynamic testing was conducted to verify the flight readiness of the Apollo docking hardwar...
One of the most critical operational functions for the space station is the orbital docking between ...
The Space Station Mechanism Test Bed consists of a hydraulically driven, computer controlled six deg...
In this paper, an analytical approach for studying the contact dynamics of space-based vehicles duri...
This paper discloses the design procedure of a docking mechanism for space applications. The mechani...
Logicon Control Dynamics develops contact dynamics models for space-based docking and berthing vehic...
The objective of the STRONG mission is the deployment of payloads from Low Earth Orbit into greater ...
This presentation describes the application of robotic and computer vision systems to validate docki...
Design and fabricate test hardware for NASA's George C. Marshall Space Flight Center (MSFC) are repo...
Proposed future space exploration, such as lunar and Martian expeditions, will require autonomous do...
The primary purpose of the OMV is to dock with orbiting payloads and then either transfer them to a ...
The soft capture system of the NASA Docking System (NDS) is a mechanism with six-degrees of freedom ...