Results 101 to 110 of about 1,938 (262)

Isometric training at longer muscle–tendon complex lengths: A potential countermeasure to impaired neuro‐muscle–tendon function during space travel

open access: yesExperimental Physiology, EarlyView.
Abstract Manned space exploration to distant destinations, including Mars, continues to be an aspiration of humankind. Space travel does, however, present many challenges to the body, amongst which adaptation to microgravity is perhaps the largest. For instance, both short and long manned spaceflight missions have shown substantial deleterious effects ...
Gerard McMahon   +2 more
wiley   +1 more source

Consensus SE(3)-Constrained Extended Kalman Filter for Close Proximity Orbital Relative Pose Estimation

open access: yesAerospace
In this paper, a recently proposed SE(3)-constrained extended Kalman filter (EKF) is extended to formulate a strategy for relative orbit estimation in a space-based sensor network. The resulting consensus SE(3)-constrained EKF utilizes space-based sensor
S. Mathavaraj, Eric A. Butcher
doaj   +1 more source

GPS-Based Real-Time Navigation for the PRISMA Formation Flying Mission [PDF]

open access: yes, 2006
The paper addresses the design, implementation and validation of the on-board navigation system for the PRISMA technology demonstration mission. The objective of the navigation system is to provide in real-time absolute and relative orbit information for
Gill, Eberhard   +3 more
core  

Spaceborne and spaceborn: Physiological aspects of pregnancy and birth during interplanetary flight

open access: yesExperimental Physiology, EarlyView.
Abstract Crewed interplanetary return missions that are on the planning horizon will take years, more than enough time for initiation and completion of a pregnancy. Pregnancy is viewed as a sequence of processes – fertilization, blastocyst formation, implantation, gastrulation, placentation, organogenesis, gross morphogenesis, birth and neonatal ...
Arun V. Holden
wiley   +1 more source

Reduced attitude synchronization of rigid spacecraft with guaranteed performance

open access: yesFranklin Open
This paper addresses the problem of reduced attitude synchronization, specifically focusing on the coordination of pointing directions between two spacecraft modeled as rigid bodies.
Geethu I., Rakesh R. Warier
doaj   +1 more source

Low magnetic disturbance analysis and testing of a novel proof mass type for gravitational reference sensor system

open access: yesAdvances in Mechanical Engineering, 2019
The proof mass used for gravitational-wave or Earth-gravity-field detection is usually comprised of materials such as gold–platinum alloys, which have a high density and low magnetic susceptibility, in order to reduce the magnetic disturbance produced by
Zeyang Zhao, Zhaokui Wang, Yulin Zhang
doaj   +1 more source

TanDEM-X Scientific Results and Future Formation Flying SAR Missions [PDF]

open access: yes, 2011
TanDEM-X (TerraSAR-X add-on for Digital Elevation Measurements) is an innovative spaceborne radar interferometer mission that was launched on June 21, 2010. This paper gives an overview of scientific experiments that have been conducted during the TanDEM-
Lopez Dekker, Paco   +9 more
core  

Analysis of Inter-Satellite Communication Protocols and their Effects on Satellite Formation Control [PDF]

open access: yes, 2011
Satellite Formation Flying (SFF) enables the collective use of multiple spacecraft to perform the function of a single, large, virtual instrument.
TORTORA, PAOLO   +2 more
core  

Dynamics Modeling of Spacecraft Formation Flying and Evaluating the Models Accuracy under the Effects of Relative Distance, Eccentricity and Earth Gravitational Perturbation [PDF]

open access: yesفصلنامه علوم و فناوری فضایی, 2012
Relative motion of satellites in a formation can be studied in several forms of dynamics models. In this paper, some of the most applicable models each implying particular assumptions, constraints and specifications are described in Cartesian and orbital
M. Navabi, M. Barati
doaj  

Application of discrete time sliding mode control to a spacecraft in 6DoF [PDF]

open access: yes
This paper presents the application of two separate discrete time sliding mode controllers, developed in conjunction with a potential function guidance method, to provide control in both position and attitude for a rigid, holonomic spacecraft body.
Veres, Sandor M., Lincoln, Nicholas K.
core  

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