EIGHTH QUARTERLY PROGRESS REPORT ON THE DEVELOPMENT OF A UNIVERSAL AUTOMATIC FLIGHT CONTROL SYSTEM AN ASW – 12(V)

摘要

Results of the RL-23 aircraft and H-21 helicopter flight test programs are presented to demonstrate the ability of the Automatic Flight Control System AN/ASW-12(V) equipped aircraft to satisfy specification requirements.nComponent environmental test data and H-37 component installation data are included.nSmooth engage circuits for the altitude control in fixed wing and helicopter installations are described and illustrated in detail.