The smart-cue and smart-gain concepts were developed as a means to alleviate pilot–vehicle-system loss of control in the presence of control surface actuator rate limiting. Both concepts exploit the measure of dynamic distortion, that is, the difference between the actual and an ideal aircraft control system response. The concept of dynamic distortion has significantly evolved in work conducted by Systems Technology, Inc., during a two-phase program sponsored by NASA Dryden Flight Research Center.Download Now
Your free whitepaper from Systems Technology, Inc. is waiting - download it now! At Systems Technology we like to say, “if it moves, we can engineer a solution to your vehicle control challenge.” We collaborate with internal engineering teams to solve complex challenges for aerospace machines - from fixed to rotary wing, conventional to eVTOL, hover to hypersonic, manned to unmanned, and piloted to autonomous.
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