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Re: AO-40 Attitude Information
- Subject: Re: [amsat-bb] AO-40 Attitude Information
- From: "Norbert Sayou" <norbert.sayou@xxxxxxxxxx>
- Date: Sat, 29 Dec 2001 15:06:50 -0300
Hello Peter and Stancey,
The S/C attitude for january 12/13 seem good for trafic.
AO40 transponder will be open for an expedition on devil island ( IOTA
SA020) with FY5KE kourou radio club ?
Happy new year
FY1DW Norbert
----- Original Message -----
From: Peter Guelzow <peter.guelzow@arcormail.de>
To: <amsat-bb@AMSAT.Org>
Sent: Saturday, December 29, 2001 2:02 PM
Subject: [amsat-bb] AO-40 Attitude Information
>
> Dear All,
>
> May I take this chance to say a big thank you to our command stations
> James Miller G3RUH, Stacey Mills W4SM, Ian Ashley ZL1AOX, Graham
> Ratcliff VK5AGR, and all those who support them with telemetry, for
> an outstanding effort in keeping AO-40 operational and work as it's best.
> Special thanks also to Paul Willmott for keeping the telemetry archive
> up to date and organizing all the mass of telemetry data.
>
> HAPPY NEW YEAR to everyone!!
>
> best wishes
> Peter
>
> --
> Peter Guelzow, DB2OS
> Pres. AMSAT-DL
>
>
>
> The following information is provided by G3RUH:
>
>
____________________________________________________________________________
__
>
> AO-40 Attitude Information
> --------------------------
> The YACE camera was activated on Orbit 535 in order to check the AO-40
> attitude.
>
> This is done every 5 orbits which also enables calibration of the excess
> precession in ALON (the so-called "Mystery Effect").
>
> Presently the Sun sensors cannot see the Sun, so the Sun/Earth sensor
system
> is unuseable. This "hibernation" commenced on orbit 529 (Dec 24) and will
> continue until orbit 549 on 2002 Jan 09 [Wed]. You can tell that this is
the
> case because the telemetered analogue spin rate is meaningless; the true
> spin rate is in fact 2.51 rpm.
>
> Today Dec 29 on orbit 535 the attitude measured ALON 327.4, ALAT -11.4
> with an uncertainty of order 0.1 deg.
>
> The attitude direction will drift as follows:
>
> Sun Illumin-
> DATE ALON ALAT Angle ation %
> ---------------------------------------------------
> 2001 Dec 20 [Thu] 347.5 -10.2 -37.2 79.7
> 2001 Dec 21 [Fri] 345.7 -10.2 -39.0 77.7
> 2001 Dec 22 [Sat] 342.2 -10.2 -41.8 74.5
> 2001 Dec 23 [Sun] 340.3 -10.3 -43.5 72.5
> 2001 Dec 24 [Mon] 338.5 -10.3 -45.1 70.6 << Sun sensor stopped
> 2001 Dec 25 [Tue] 336.6 -10.3 -46.5 68.8 .. .. ..
> 2001 Dec 26 [Wed] 333.1 -10.3 -48.6 66.2 .. .. ..
> 2001 Dec 27 [Thu] 331.3 -10.3 -49.7 64.7 .. .. ..
> 2001 Dec 28 [Fri] 329.5 -10.4 -50.7 63.4 .. .. ..
> 2001 Dec 29 [Sat] 327.6 -10.4 -51.5 62.3 .. .. ..
> 2001 Dec 30 [Sun] 324.1 -10.4 -52.3 61.1 .. .. ..
> 2001 Dec 31 [Mon] 322.3 -10.4 -52.7 60.6 .. .. ..
> 2002 Jan 01 [Tue] 320.4 -10.4 -52.9 60.4 .. .. ..
> 2002 Jan 02 [Wed] 318.6 -10.4 -52.8 60.4 .. .. ..
> 2002 Jan 03 [Thu] 315.1 -10.5 -52.3 61.2 .. .. ..
> 2002 Jan 04 [Fri] 313.2 -10.5 -51.8 61.9 .. .. ..
> 2002 Jan 05 [Sat] 311.4 -10.5 -51.1 62.8 .. .. ..
> 2002 Jan 06 [Sun] 309.6 -10.5 -50.2 64.0 .. .. ..
> 2002 Jan 07 [Mon] 306.1 -10.5 -48.4 66.4 .. .. ..
> 2002 Jan 08 [Tue] 304.2 -10.6 -47.2 68.0 .. .. ..
> 2002 Jan 09 [Wed] 302.4 -10.6 -45.8 69.7 << Sun sensor restarts
> 2002 Jan 10 [Thu] 300.5 -10.6 -44.3 71.5
> ..
> ---------------------------------------------------
>
> On Jan 09, when the Sun sensor recovers lock, the magnetorquer will be
used
> once again to:
>
> a) counteract the "mystery effect" precession (drift) in alon
> b) to drive alat towards alat=0
> c) increase alon towards alon=360 as rapidly as the Sun's movement
allows.
>
> Broadly the future should be:
>
> Date Alon Alat
> -----------------------
> 2002 Jan 08 300 -10
> 2002 Jan 15 300 -5
> 2002 Jan 22 300 0
> 2002 Feb 19 320 0
> 2002 Mar 19 340 0
> 2002 Apr 13 360 0
> -----------------------
>
> Excellent communications are available now, and will be maintained
throughout
> this period.
>
> JRM 2001 Dec 29 [Sat] 1414 utc
>
____________________________________________________________________________
__
>
> ----
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