With an entirely new thrust vectoring system, Scout V 0.8 corrected well for it's orientation with two caveats. The first being that due to errors within a computer simulation of the flight, the liftoff weight was much too heavy to allow for a suitable apogee. The second being that the onboard PID system was running for roughly 30 seconds before liftoff, and too much error was accumulated during that time to maintain a zero-position in the TVC mount.