An assistance system for pilot at landing approach

For every civil pilot, the landing approach to the target runway is one of the most difficult operations. The pilot should predict the touch point of landing, the vertical speed, and the horizontal speed at the point. In the most case, there is a wind with some degree of speed through the approach. The pilot should calculate the effect of the wind in the approach. The proposing assistance system in this paper is a display system in which the prediction of trajectory of the approaching civil airplane is forecasted in the synthetic views on a tablet computer. The tablet computer is separated from the control system of the airplane, so that the tablet computer should acquire the positional information and the acceleration values only from the own GPS module and the own acceleration sensors. The practical effectiveness of the proposing assistance system will be evaluated through the usual uses by civil pilots.