![primary flight control system primary flight control system](http://1.bp.blogspot.com/-JbpiouOwIfA/U7lGxyy6rdI/AAAAAAAACqQ/VjxsAPu4vDs/s1600/Transferring+control+surface+inputs+from+the+cockpit.jpg)
2 promising approaches are versatile wings, and fluidics. advanced combat rotorcraft flight-control systems to help bridge this technology gap. Several technology analysis and development efforts exist to integrate the functions of control systems like ailerons, elevators, elevons, flaps, and flaperons into wings to perform the mechanics purpose. Secondary flight managements embrace control of flap and slat systems, freelance control and monitor architectures and extremely integrated electronic management schemes. Secondary flight control systems, conjointly referred to as high lift flight controls, enhance an aircraft’s mechanics performance beneath certain flight conditions. Fly-by-wire control systems enable automatic functions like aircraft stability, and provide redundancy in both computers and electronics to maximise safety and dependability. Primary flight control systems offer operation for the aircraft’s airfoil, elevator, rudder, spoiler and horizontal stabiliser trim actuator (HSTA).Fly-by-wire technology, electro-hydrostatic actuation (EHA) and electro-backup hydrostatic actuation (EBHA) are currently taking the lead over hydro-mechanical control systems. This was the first type of flight control system developed and is still in use today in some. (PFCS) reliability and mainte- nance study was one of five tasks of contract. Here are four types of flight control systems in the order they were developed: Mechanical flight control system: in this type of flight control system, there are mechanical linkages between the pilot command inputs and the various flight controls. The fundamentals of craft controls area unit explained in flight dynamics. The Boeing model 747 primary flight control system. Aircraft engine controls also are thought of as flight controls as they alter speed. The actuators are controlled in unison by a single cable and linkage transmission path which connects to the rudder pedals. Aircraft control system consists of control surfaces, the individual cockpit controls, connecting linkages, and also the necessary operational mechanisms to regulate an aircraft's direction on the wing. yaw control system Yaw control (Figure 1-16) is provided by two rudders, which are individually driven by independent hydraulic actuators. Aircraft Control System is a congregation of machine-driven and electronic equipage which concedes an aircraft to be flown with exceptional rigor and constancy.