guidance, flight mechanics and trajectory optimization
guidance, flight mechanics and trajectory optimization
guidance, flight mechanics and trajectory optimization
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Figure 4.3<br />
Velocity Increments to Rendezvous (Ref. 4a)<br />
Initial Conditions, 1 = 139,000 ft = 42.3 km,<br />
2 = 72,300 ft = 22.0 km,<br />
3 = 335. ft/ set= 104. m/set<br />
4 = 170 ft/sec = 51.7 m/set<br />
C”.RAC7L”I87IC I I<br />
VLLOCITY<br />
lCC8I<br />
Figure 4.4<br />
Velocity Increments to Rendezvous (Ref 4a)<br />
Initial Conditions, Tl = T2 = 60,000 ft = 18.3 h<br />
VELoCIl<br />
(FPSI<br />
713 = -100 ft/sec = -305 m/set<br />
74 = -350 ft/ set = 107 m/set<br />
70<br />
I/ I II i<br />
TIME ISECONDS)<br />
Wl.PI
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