guidance, flight mechanics and trajectory optimization
guidance, flight mechanics and trajectory optimization
guidance, flight mechanics and trajectory optimization
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.<br />
0<br />
i<br />
time difference between a reference time, to, <strong>and</strong> current time<br />
unit vectors of rotating coordinate systems centered at the rendez-<br />
vous vehicle<br />
unit vectors of a rotating coordinate .system centered at the rendez-<br />
vous vehicle<br />
acceleration (control)<br />
velocity<br />
components along the u,v,w or u<br />
--- -l,xl,wl unit vectors<br />
.<br />
components along the P,Q,W unit vectors<br />
true anomaly<br />
gravitational constant of attracting body<br />
components of the relative position vector (e)<br />
position vector between target <strong>and</strong> rendezvous vehicle<br />
22<br />
dt<br />
3<br />
dM<br />
d<br />
dB<br />
d<br />
dE<br />
denotes a vector quantity<br />
denotes a vector quantity<br />
SUPERSCRIPTS<br />
SUBSCRIPTS<br />
denotes the ith component of a vector