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- From: mrw9e@kelvin.seas.Virginia.EDU (Michael Robert Williams)
- Subject: Re: Orbital motion question
- Message-ID: <1992Dec14.173003.1832@murdoch.acc.Virginia.EDU>
- Sender: usenet@murdoch.acc.Virginia.EDU
- Organization: University of Virginia
- References: <1ggfesINN29q@access.usask.ca>
- Date: Mon, 14 Dec 1992 17:30:03 GMT
- Lines: 32
-
- In article <1ggfesINN29q@access.usask.ca> choy@skorpio.usask.ca (I am a terminator.) writes:
- >
- >Let the vector r be the position of a mass m orbiting in a plane around
- >another mass M (which doesn't move) at the origin. The mass m is
- >accelerated such that
- >
- > 2
- > d r KMm
- >m --- = - ---- r
- > 2 2
- > dt |r|
- > r
- > d---
- > |r|
- >What is the scalar product of r/|r| and ------ ?
- > dt
- >
- >If m moved in an elliptical path, can the scalar product be zero?
- >
-
- The scalar product of r/|r| and d(r/|r|)/dt is called sigma, and is
- always zero for a circular orbit, but has different values for each point
- on an elliptical, parabolic or hyperbolic orbit. sigma is equal to
- zero at the peri- and apo-apsis of any orbit, regardless of type. If
- you divide sigma by the magnitudes of r/|r| and d(r/|r|)/dt, you get
- the cosine of a quantity called the flight path angle.
-
-
- In Real Life:Mike Williams | Perpetual Grad Student
- e-mail :mrw9e@virginia.edu| - It's not just a job, it's an indenture
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