Astrodynamics 102 - DerAstrodynamics.com
Astrodynamics 102 - DerAstrodynamics.com
Astrodynamics 102 - DerAstrodynamics.com
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Numerical Example 5<br />
ICBM transfer orbit , Single revolution 2-Body, Vinti targeting, Kepler+ targeting solutions<br />
Input:<br />
clock1 = at t1 (needed for Lambert+)<br />
inc_to = 1, (inclination of transfer orbit < 90 deg.), t1 = 0., t2 = 1618.50 (seconds)<br />
Output:<br />
* <strong>com</strong>puted inclination of transfer orbit = 67.895 deg., transfer angle = 296.368 deg.<br />
Algs. Rev# v_eci (t1) (km/s) v_eci (t2) (km/s)<br />
2-Body N =0 <br />
Vinti<br />
_targeting<br />
r_eci (t1) (km) r_eci (t2) (km)<br />
<br />
N = 0 <br />
Lambert+ N = 0 <br />
*
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