نتایج جستجو برای: spacecraft equipment

تعداد نتایج: 87564  

2004
Rob Sherwood Steve A. Chien Daniel Tran Benjamin Cichy Rebecca Castaño Ashley Davies Gregg Rabideau

An Autonomous Science Agent is currently flying onboard the Earth Observing One Spacecraft. This software enables the spacecraft to autonomously detect and respond to science events occurring on the Earth. The package includes software systems that perform science data analysis, deliberative planning, and run-time robust execution. Because of the deployment to a remote spacecraft, this Autonomo...

2003
Roberto Lampariello Sunil Kumar Agrawal Gerd Hirzinger

This paper addresses the problem of motion planning for free-flying robots. Full state actuation is considered to allow for large displacements of the spacecraft. Motion planning is formulated as an optimization problem and kinematic as well as dynamic constraints are considered. The chosen optimization criteria are spacecraft actuation and final time. The proposed method allows solutions which...

2002
Y. Fang

In this paper, we design a nonlinear controller for the kinematic model of an underactuated rigid spacecraft that ensures uniform, ultimately bounded (UUB) tracking provided the initial errors are selected sufficiently small. The result is achieved via a judicious formulation of the spacecraft kinematics and the novel design of a Lyapunov-based controller. We also discuss how standard backstepp...

2010
Rita Almeida Ribeiro Tiago C. Pais Luís F. Simões

In this paper we discuss the benefits of using full reinforcement operators for site selection in spacecraft landing on planets. Specifically we discuss a modified Uninorm operator for evaluating sites and a Fimica operator to aggregate pixels for constructing regions that will act as sites to be selected at lower spacecraft altitude. An illustrative case study of spacecraft target landing is p...

2006
Hyochoong Bang

A new approach for spacecraft maneuver based upon constraint dynamics and tracking control laws is presented in this paper. For high precision pointing requirement on spacecraft maneuver, a desired trajectory is prescribed upon which a constraint dynamic system is constructed. A reference model system governed by constraint force is used to build the associated control laws for actual system. S...

Journal: :Applied sciences 2023

Scientific payloads onboard CubeSats usually have complex geometries and occasionally narrower allowed temperature ranges with respect to the rest of spacecraft. In these cases, capability correctly predict thermal behaviour payload once in orbit is mandatory. To achieve this ability, a balance test required identify model payload. The consists application different external boundary conditions...

2016
Mina Bashir Mahjabeen Ahmed Thomas Weinmaier Doina Ciobanu Natalia Ivanova Thomas R. Pieber Parag A. Vaishampayan

Strict planetary protection practices are implemented during spacecraft assembly to prevent inadvertent transfer of earth microorganisms to other planetary bodies. Therefore, spacecraft are assembled in cleanrooms, which undergo strict cleaning and decontamination procedures to reduce total microbial bioburden. We wanted to evaluate if these practices selectively favor survival and growth of ha...

2015
Josh Newman Robert E. Zee

Specialized drift recovery and station keeping algorithms were developed for the Canadian Advanced Nanospace eXperiments 4 and 5 (CanX-4 & CanX-5) formation flying mission (launched 30 June 2014), and successfully verified on orbit. These algorithms performed almost exactly according to predictions. The highly successful CanX4 and CanX-5 formation flying demonstration mission was completed in N...

2011
M. W. Dunlop Q.-H. Zhang Y. V. Bogdanova K. J. Trattner Z. Pu H. Hasegawa J. Berchem M. G. G. T. Taylor M. Volwerk J. P. Eastwood B. Lavraud C. Shen J.-K. Shi J. Wang D. Constantinescu A. N. Fazakerley H. Frey D. Sibeck P. Escoubet J. A. Wild Z. X. Liu

During April to July 2007 a combination of 10 spacecraft provided simultaneous monitoring of the dayside magnetopause across a wide range of local times. The array of four Cluster spacecraft, separated at large distances (10 000 km), were traversing the dawn-side magnetopause at high and low latitudes; the five THEMIS spacecraft were often in a 4 + 1 grouped configuration, traversing the low la...

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