GUST COMPENSATION FOR ANGLE-OF-ATTACK REFERENCE AIRCRAFT SPEED CONTROL SYSTEM

摘要

A system for deriving signals proportional to horizontal and vertical wind gust level each as the difference between an atmospheric measurement and an inertial reference and, by a threshold sensitive signal translator responsive only to negative ones of the derived signals, to subtract gust bias signals from the system angle-of-attack reference to compensate for those gust components which tend to reduce lift.