Elements and Parameters of the Osculating Orbit and Their Derivatives
Overview & Synopsis
The analysis determines the time derivatives of the conic-section orbital elements in a disturbed orbit by perturbation methods. Integration of any of the several resulting systems of six first-order linear differential equations by numerical methods can be a useful tool for the solution of problems in orbital mechanics. Equations for the two-body orbit are also summarized in a convenient manner.
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ntrs.nasa.gov)
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Document Information
| Document Title | Elements and Parameters of the Osculating Orbit and Their Derivatives |
|---|---|
| Author / Organization | Wilbur F Dobson, Vearl N Huff, Arthur V Zimmerman |
| Subject & Discipline | OTHER |
| Categories | Aerospace & Aviation |
| Publication Year | 1996 |
| License / Rights | Public Domain / NASA STI Open Access |
| Resource Verification | Listed PDF (Verification Pending) |
| Original Host Website |
NASA Technical Reports Server
(ntrs.nasa.gov)
|
| File Format | application/pdf (Portable Document Format) |
| Language | EN |
| Catalog ID | DOC-67001 |
| Original Source Link | Visit Source Page on ntrs.nasa.gov » |