Results 261 to 270 of about 4,818 (307)
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Journal of Geophysical Research: Solid Earth, 1990
The average drag on the LAGEOS satellite appears to be well understood. It consists of three types of drag: Yarkovsky thermal, neutral particle, and charged particle. Yarkovsky thermal drag depends on the LAGEOS spin axis position. The spin axis in the decade since launch appears to have stayed near where the engineering telemetry data put it at apogee
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The average drag on the LAGEOS satellite appears to be well understood. It consists of three types of drag: Yarkovsky thermal, neutral particle, and charged particle. Yarkovsky thermal drag depends on the LAGEOS spin axis position. The spin axis in the decade since launch appears to have stayed near where the engineering telemetry data put it at apogee
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Robust Digital Control of Drag-Free Satellites
IFAC Proceedings Volumes, 2003Abstract A drag-free satellite is a small proof-mass (PM) shielded by a spacecraft cavity and moving only subject to gravitational forces. This can be accomplished by a drag-free control keeping the PM centered in the cavity and compensating the non-gravitational forces acting on the spacecraft. A constellation of drag-free satellites can be employed
CANUTO, Enrico, ANDREIS D.
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Drag coefficients for tumbling satellites.
Journal of Spacecraft and Rockets, 1967Figure 3 shows how typical PLOT results are presented. For illustrative purposes, ROD is plotted as a function of normal countdown time, which is extended by the programmed hold. Gain in PLOT is plotted as a function of programmed hold-time; the gain is referenced to RCD for the normal countdown.
LEE H. SENTMAN, STANFORD E. NEICE
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Stability of Gravity-Stabilized Drag-Free Satellites
AIAA Journal, 1971In a drag-free satellite, the relative position sensor null point and the thrustor lines of action will not be coincident with the vehicle mass center. Thus, attitude motion is sensed by the translation control system. The resulting coupling between the attitude and translational motions can cause attitude instabilities in a gravity stabilized drag ...
Fleming, Alan W., DeBra, Daniel B.
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Embedded Model Control Application to Drag-Free and Satellite-to-Satellite Tracking
2006 14th Mediterranean Conference on Control and Automation, 2006This paper describes the realization of a generic simulator for formation flying satellites, and the design and application of Embedded Model Control (EMC) to the spacecraft control, as potentially applicable to a constellation of drag-free satellites.
MASSOTTI, Luca +2 more
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Attitude and Drag Control: An Application to the GOCE Satellite
2003The Gravity held and steady-stale Ocean Circulation Explorer (GOCE) satellite, currently planned to be launched in the course of 2006, will require a precise drag compensation and a fine attitude control along the Local Orbiting Reference Frame (LORF) of a polar Sun-synchronous low orbit, allowing the Earth gravity field to be recovered with ...
CANUTO, Enrico, MARTELLA P, SECHI G.
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Satellite Drag Perturbations in an Oblate Diurnal Atmosphere
AIAA Journal, 1975Analytic expressions are derived that describe decay rates in period and eccentricity, and rotation in perigee argument for orbits of small eccentricity ...
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Interferometric sensing for drag-free satellites
SPIE Proceedings, 2004ABSTRACT We discuss a polarisation based homodyne interferometer that demonstrates a promising sensitivity of approximately. This performance figure is limited above 10 Hz by the resolution of the current analogue-to-digitalconverter (ADC). Sensitivity below 10 Hz is influenced by environmental factors a nd / or noise inherent in the laser.
Clive C. Speake, Stuart M. Aston
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The Effect of Atmospheric Drag on the Orbit of an Arfificial Satellite
The Mathematical Gazette, 1969The study of artificial satellites is today a subject of topical interest and naturally much work has been completed in the field of satellite orbits. Many aspects of this work involve the use of differential equations. Unfortunately very few of these may be solved by ordinary analytic techniques.
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2008
Scientific satellite missions trying to investigate questions regarding geodesy and fundamental physics have become increasingly dependent on ultra low disturbance environments. The precision demanded by the experiments has risen continuously as experimenters strive to deepen their understanding.
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Scientific satellite missions trying to investigate questions regarding geodesy and fundamental physics have become increasingly dependent on ultra low disturbance environments. The precision demanded by the experiments has risen continuously as experimenters strive to deepen their understanding.
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