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The determination of orbits using picard iteration
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Feagin, T. Mikkilineni, R. P. |
| Copyright Year | 1975 |
| Description | The determination of orbits by using Picard iteration is reported. This is a direct extension of the classical method of Picard that has been used in finding approximate solutions of nonlinear differential equations for a variety of problems. The application of the Picard method of successive approximations to the initial value and the two point boundary value problems is given. |
| File Size | 241544 |
| Page Count | 8 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760003080 |
| Archival Resource Key | ark:/13960/t05x73k05 |
| Language | English |
| Publisher Date | 1975-08-01 |
| Access Restriction | Open |
| Subject Keyword | Astrodynamics Boundary Value Problems Approximation Orbital Position Estimation Iterative Solution Flight Mechanics Orbit Calculation Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |