With an entirely new thrust vectorin' system, Scout V 0.8 corrected well for it's orientation with two caveats. T' first bein' that due t' errors within a computer simulation o' t' flight, me hearties, t' liftoff weight was much too heavy t' allow for a suitable apogee. T' second bein' that t' onboard PID system was runnin' for roughly 30 seconds before liftoff, me hearties, and too much error was accumulated durin' that time t' maintain a zero-position in t' TVC mount.