In the special case of constant acceleration, there is a nice coordinate system, Rindler coordinates, but if the acceleration is nonconstant, then it's pretty hopeless to come up with a coordinate system in which the rocket is always at rest. For instance, if the rocket accelerates for a while, drifts for a while, decelerates, then drifts back to where it started, there is no good way to describe that using a noninertial coordinate system. The way you have to describe situations like that is either to use inertial coordinates, where the rocket is not at rest, or else use charts, which are coordinate systems that only apply to small regions of spacetime. (Then you have to worry about relating coordinates of one chart with coordinates of the other).