Perspective predictor/flight-path display with minimum pilot compensation

Prediction can substantially enhance the novel guidance and control capabil ities of perspective flight-path displays. A position predictor based on ge ometry/kinematics relations is considered and an extension based on manual control theory issues is introduced. Pilot-centered requirements for compen sation control of the predictor-aircraft system are considered. It is shown which are the effects on pilot-predictor aircraft system crossover, system stability, response quality, and system bandwidth. A solution for a predic tor with optimum pilot compensation is presented. furthermore, it is shown that the flight-path predictor is also an existent means for controlling th e current state of the aircraft. The conceptual and theoretical predictor c onsiderations are verified with pilot-in-the-loop simulation experiments.