Results 181 to 190 of about 15,749 (218)

Emerging roles for the nucleolus in development and stem cells.

Development
Leeke BJ, Staffhorst I, Percharde M.
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Advancing bridge resilience: a review of monitoring technologies for flood-prone infrastructure. [PDF]

Open Res Eur
Buka-Vaivade K, Nicoletti V, Gara F.
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Review of the Application of UAV Edge Computing in Fire Rescue. [PDF]

Sensors (Basel)
Sun H, Xu R, Luo J, Cheng H.
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Chromatin Protection by the Chromosomal Passenger Complex

Gireesh A, Abad M, Nozawa R, Sotelo-Parrilla P, Dury L, Likhodeeva M, Spanos C, Peralta CC, Rappsilber J, Hopfner K, Wilson M, Vanderlinden W, Hirota T, Jeyaprakash A.   +13 more
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High-resolution vertical profiling of aerosols microphysical and optical properties during the 2024 LEADER UAV campaign in Nadarzyce (Poland). [PDF]

Environ Sci Pollut Res Int
Markowicz KM, Chiliński MT, Panfil W, Nurowska K, Moczulski W, Makuch P, Acedański S, Florczyk GM, Kozuba J.   +8 more
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Senescence-driven solubilization of biomass is the main source of kelp-derived dissolved organic carbon to the coastal ocean. [PDF]

Commun Biol
English CJ, Bell TW, Opalk K, Siegel DA, Carlson CA.   +4 more
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Global re-organisation of genome architecture at the transition to gametogenesis

Huang T, Rigau M, Malysheva V, Whildling C, Siciliani S, Li J, Balaguer Balsells I, Artemov P, Dion C, Spivakov M, Vaquerizas JM, Hajkova P.   +11 more
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Tether satellite system collision study

Acta Astronautica, 1999
A study was performed to determine the probability of collision with resident space objects and untrackable debris for the tether component of the Tethered Satellite System (TSS) after it broke away from the Space Shuttle orbiter (mission STS-75) in February 1996.
V.A. Chobotov, D.L. Mains
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Three-dimensional vibrations of tethered satellite systems

Journal of Guidance, Control, and Dynamics, 1991
The three-dimensional free vibrations of an orbiter-towed tethered satellite system with nominally vertical tether during stationkeeping phase are studied analytically. The tether is modeled as an elastic continuum with mass and the orbiter and the subsatellite as two concentrated masses.
PASCA M, PIGNATARO M, LUONGO, Angelo
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Tethered Satellite System control system design

3rd Tethers in Space/ Toward Flight International Conference, 1989
This paper discusses the control aspects of the Tethered Satellite System mission. The deployer controls system uses length-error and tension-error feedback to control in-plane libration, length, and length rate. The satellite's reaction control system is used to augment tether tension, control rates and attitude about the tether axis, and to damp in ...
DONALD TOMLIN, DAVID MOWERY, CARL BODLEY
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