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Methods for calculating the navigation information for mars spacecraft
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Elyasberg, P. E. Aleksashin, N. G. Khavenson, N. G. |
| Organization | The National Aeronautics and Space Administration (NASA) |
| Copyright Year | 1973 |
| Abstract | METHODS USED TO CALCULATE NAVIGATION PARAMETERS FOR INTERPLANETARY MARS SPACECRAFT ARE DISCUSSED. THE METHODS ARE BASED ON THE NUMERICAL INTEGRATION OF THE DIFFERENTIAL EQUATIONS OF MOTION OF THE SPACECRAFT. TO CALCULATE THE POSITION OF CELESTIAL BODIES, NEWCOMB EXPANSIONS ARE USED IN THE CASE OF PLANETS AND POLYNOMIALS BASED ON BROWN'S THEORY IN THE CASE OF THE MOON. THE METHODS CAN BE USED FOR NAVIGATIONAL CALCULATIONS OF ANY INTERPLANETARY SPACECRAFT IN THE EARTH-MARS OR EARTH-MOON SPACE. |
| File Size | 768604 |
| File Format | |
| Alternate Webpage(s) | http://www.archive.org/details/nasa_techdoc_19730016977 |
| Archival Resource Key | ark:/13960/t9h42ft82 |
| Language | English |
| Publisher Date | 1973-05-01 |
| Access Restriction | Open |
| Subject Keyword | Airfoil Profiles Boundary Layer Separation Kutta-joukowski Condition Three Dimensional Flow Vortex Sheets Aerodynamic Characteristics Flow Characteristics Flow Equations Numerical Analysis Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
