guidance, flight mechanics and trajectory optimization
guidance, flight mechanics and trajectory optimization
guidance, flight mechanics and trajectory optimization
Create successful ePaper yourself
Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.
where<br />
(= constant rocket motor thrust<br />
M =' instantaneous mass = MO - Mt<br />
t= direction of rocket thrust referenced to the<br />
F./&’<br />
Coordinate Definition<br />
Figure 4.8<br />
The solution to this set of equations is<br />
81<br />
1<br />
RJNDEZVOUS<br />
VEHICLE