Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Akil J Middleton"'
Autor:
Kevin R Duda, Rebecca A Vasquez, Akil J Middleton, Mitchell L Hansberry, Dava J Newman, Shane E Jacobs, John J West
Publikováno v:
Frontiers in Systems Neuroscience, Vol 9 (2015)
The Variable Vector Countermeasure Suit (V2Suit) for Space Habitation and Exploration is a novel system concept that provides a platform for integrating sensors and actuators with daily astronaut intravehicular activities to improve health and perfor
Externí odkaz:
https://doaj.org/article/34a3d4d89f52425d904116f1b432d5ff
Publikováno v:
2015 IEEE Aerospace Conference.
The Variable Vector Countermeasure Suit (V2Suit) is a countermeasure suit for sensorimotor adaptation and musculoskeletal deconditioning in microgravity. The V2Suit consists of wearable modules containing arrays of control moment gyroscopes (CMGs) th
Autor:
Akil J. Middleton, Rebecca A. Vasquez, John J. West, Dava J. Newman, Kevin R. Duda, Shane E. Jacobs, Mitchell L. Hansberry
Publikováno v:
Frontiers Research Foundation
Frontiers in Systems Neuroscience
Frontiers in Systems Neuroscience, Vol 9 (2015)
Frontiers in Systems Neuroscience
Frontiers in Systems Neuroscience, Vol 9 (2015)
The “Variable Vector Countermeasure Suit (V2Suit) for Space Habitation and Exploration” is a novel system concept that provides a platform for integrating sensors and actuators with daily astronaut intravehicular activities to improve health and
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::74d78654b68593ed70405a1af0086f1c
http://hdl.handle.net/1721.1/97066
http://hdl.handle.net/1721.1/97066
Publikováno v:
2014 IEEE Aerospace Conference.
The Variable Vector Countermeasure Suit (V2Suit) is a wearable intravehicular system that will provide a viscous resistance to movements that are parallel to a specified direction of ‘down.’ The V2Suit utilizes control moment gyroscopes (CMGs) in
Autor:
Stephen Paschall, Akil J. Middleton
Publikováno v:
2011 Aerospace Conference.
This paper describes the development of a detailed model of the TALARIS hopper and demonstrates its performance1,2. TALARIS (Terrestrial Artificial Lunar And Reduced gravIty Simulator) is a small prototype hopping vehicle currently being developed in
Publikováno v:
2010 IEEE Aerospace Conference.
The goal of this paper is to describe a first-order performance analysis of a lunar hopper 1,2. A hopper is a vehicle that has both landing and surface mobility capabilities on a single platform. Unlike rovers, which traverse the lunar surface while