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SLR-Mail No.990

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Date:2002-10-28 12:06:00
Sender:Remko Scharroo (remko@deos.tudelft.nl) <EDC slrmail account <slrmail@dgfi.badw.de>>
Subject:[SLR-Mail] No. 990: EGS/AGU/EUG Session on Surface Forces and Rotational Dynamics
Author:Remko Scharroo
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SLR Electronic Mail 2002-10-28 12:06:00 UTC Message No. 990
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Author: Remko Scharroo (remko@deos.tudelft.nl)
Subject: EGS/AGU/EUG Session on Surface Forces and Rotational Dynamics

Dear Colleagues,

The web pages and session descriptions for the EGS/AGU/EGU Joint
Assembly in Nice, France, 6-11 April 2003 is now on-line on:
http://www.copernicus.org/egsagueug/
We would particularly like to draw your attention to Session G16
”Satellite Surface Forces and Satellite Rotational Dynamics”. The
description of the session is attached below.

Note the various deadlines for registration and abstract submission:
- Deadline for Support Application: 1 December 2002
- Deadline for ”Early Bird” Registration: 31 December 2002
- Deadline for Receipt of Abstracts: 15 January 2003
- Deadline for Pre-Registration: 7 March 2003
So remember to submit your abstract no later than 15 January.

Best regards, and hoping to see you in Nice in April,
Remko Scharroo (convener)
Douglas Currie, Frank Lemoine (co-conveners)

(PS: Excuse us if you receive this mail through various channels)
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G16 Satellite Surface Forces and Satellite Rotational Dynamics
(co-sponsored by GI)

While gravity models are rapidly improving, surface forces are becoming
the largest source of satellite orbit errors for a large range of
orbital altitudes. For low-flying satellites atmospheric drag is not
only a significant force, it is also difficult to model. Deficiencies
in drag modelling are the result of uncertainties in the density and
composition of the atmosphere, the interaction between the atmospheric
particles and the satellite surface, and motion of the atmosphere.
Particularly during periods of high solar activity, the density and
composition of the atmosphere at the satellite altitude can vary
rapidly, to as much as an order of magnitude within a few hours.

For satellites in higher orbits, drag becomes less important, while
solar radiation pressure becomes increasingly important compared to
gravity. The major source of uncertainty in radiation pressure
modelling are the reflective properties of the satellite surface, and,
for satellites without attitude control and monitoring, the attitude.
In the case of LAGEOS I and II, significant advances have been made
recently to model the attitude, with important implications for the
surface force modelling.

Because of their close interaction, both satellite surface forces and
rotational dynamics are the topic of this session. We particularly
welcome papers dealing jointly with both subjects. Encouraged are also
submissions dealing with new methods for modelling of atmospheric drag,
the interaction between particles or photons and the satellite surface,
the dependence on solar activity, modelling of Earth albedo, and despin
and spin axis orientation of geodetic satellites.


Event Information


While gravity models are rapidly improving, surface forces are becoming
the largest source of satellite orbit errors for a large range of
orbital altitudes. For low-flying satellites atmospheric drag is not
only a significant force, it is also difficult to model. Deficiencies
in drag modelling are the result of uncertainties in the density and
composition of the atmosphere, the interaction between the atmospheric
particles and the satellite surface, and motion of the atmosphere.
Particularly during periods of high solar activity, the density and
composition of the atmosphere at the satellite altitude can vary
rapidly, to as much as an order of magnitude within a few hours.

For satellites in higher orbits, drag becomes less important, while
solar radiation pressure becomes increasingly important compared to
gravity. The major source of uncertainty in radiation pressure
modelling are the reflective properties of the satellite surface, and,
for satellites without attitude control and monitoring, the attitude.
In the case of LAGEOS I and II, significant advances have been made
recently to model the attitude, with important implications for the
surface force modelling.

Because of their close interaction, both satellite surface forces and
rotational dynamics are the topic of this session. We particularly
welcome papers dealing jointly with both subjects. Encouraged are also
submissions dealing with new methods for modelling of atmospheric drag,
the interaction between particles or photons and the satellite surface,
the dependence on solar activity, modelling of Earth albedo, and despin
and spin axis orientation of geodetic satellites.

From: EDC slrmail account

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