hw09_FA05 - a,e,i Ω and ω •(10 pts DCM C EP which...

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R.G. Melton AERSP 309 HW #9 Fall 2005 (due at beginning of class Monday Nov. 14) (55 points) Write a computer program (Fortran, C, C++, Matlab, Mathematica, Mathcad, or Basic) that a. (5 pts) takes as input a position vector (km) and a velocity vector (km/s) in ECI coordinates for an Earth orbit b. (5 pts) echoes these input values to the output, along with labels and units c. calculates and outputs (with labels and units) the (15 pts) orbital elements
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Unformatted text preview: a,e,i, Ω , and ω • (10 pts) DCM C EP which converts from system E (ECI coordinates) to system P (perifocal coordinates) • (10 pts) position and velocity vectors in perifocal coordinates d. (10 pts) Run the program using the input vectors below. Hand in a listing of your program and the printed output. ) / ( ˆ 002 . 2 ˆ 230 . 2 ˆ 632 . 3 ) ( ˆ 13486 ˆ 9644 ˆ 11896 1 1 s km K J I v km K J I r − + − = + + = K K...
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This note was uploaded on 07/23/2008 for the course AERSP 309 taught by Professor Melton during the Fall '05 term at Penn State.

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