Introduction
For the specification of the control of an aircraft, other parameters and equipment’s other than the basic aircraft control are required. This is because there are various dynamic performance criteria that need to be factored in the aircraft control system design.
The basic aircraft system requires a navigation and control so that it works efficiently. The basic structure of the aircraft system is identified as below with the various parts performing various functions:
Aircraft system block diagram
The stability augmentation and transient response improvement are provided by the estimation control of the linear feedback block of the system. The forward loop provides ...