초록 ▼

A display system for use in an aircraft control wheel steering system provides the pilot with a single, quickened flight path angle display to overcome poor handling qualities due to intrinsic flight path angle response lags, while avoiding multiple information display symbology. The control law for

A display system for use in an aircraft control wheel steering system provides the pilot with a single, quickened flight path angle display to overcome poor handling qualities due to intrinsic flight path angle response lags, while avoiding multiple information display symbology. The control law for the flight path angle control system is designed such that the aircraft\s actual flight path angle response lags the pilot\s commanded flight path angle by a constant time lag tt

대표청구항 ▼

A method of producing a flight path angle display for an aircraft, the method comprising the steps of: (a) providing an aircraft flight control steering system having a predetermined time response lag tgDgD having a predetermined relationship to said response lag tgSYNT, where: gSYNT=gDgD; and, (e)

A method of producing a flight path angle display for an aircraft, the method comprising the steps of: (a) providing an aircraft flight control steering system having a predetermined time response lag tgDgD having a predetermined relationship to said response lag tgSYNT, where: gSYNT=gDgD; and, (e) displaying said gSYNT signal.