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Re: Satellite orbit procedure [message #29655 is a reply to message #29582]

Thu, 28 February 2002 08:32

Ed Wright
Messages: 39
Registered: February 1999

Member

in article 3C7E3189.88B08ED3@dlr.de, Richard Lord at Richard.Lord@dlr.de
wrote on 2/28/02 5:32 AM:

>
> Hi,
>
> I'm looking for a procedure that takes as input the parameters of a
> satellite orbit (Kepler orbit parameters), and outputs so-called
> statevectors. A statevector contains the x,y,z and vx,vy,vz
> coordinates at any particular point in time.
>
> If anybody has seen a procedure that does something along the lines
> explained above, I would be grateful to receive a copy.
>
> Thanks in advance,
> Richard

Give me another month and I'll finish testing a dlm interface to the JPL
CSPICE library. The library includes routines for orbit computations, time
conversion, and associated functions.

As always,
Ed Wright
JPL/NAIF

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[Message index]

		Re: Satellite orbit procedure By: Craig Markwardt on Wed, 06 March 2002 06:50
		Re: Satellite orbit procedure By: Liam E. Gumley on Wed, 06 March 2002 06:58
		Re: Satellite orbit procedure By: Ed Wright on Thu, 28 February 2002 08:32

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