Flight Control System - Scenario Part 5

As the Controller Computer demands a direction that requires a slower vertical velocity, the Perturbation Computer demands less lift. In response, the blades reduce angle of attack and camber. The blades will use negative camber and angle of attack as necessary to provide net negative lift as commanded by Perturbation Computer in response to direction and velocity demands of the Controller Computer that require negative vertical velocity in excess of that achievable with the acceleration due to gravity.