Flight Control System Advances for Near-Future Military Aircraft

1973 ◽  
Author(s):  
P. E. Blatt
Keyword(s):  
Control System ◽  
Flight Control ◽  
Flight Control System ◽  
Military Aircraft ◽  
Near Future

Flight Simulation of Military Aircraft Systems

1993 ◽  
Vol 207 (2) ◽  
pp. 127-131
Author(s):  
J E Perrin
Keyword(s):  
Control System ◽  
Design Process ◽  
Flight Control ◽  
Early Stage ◽  
Flight Simulation ◽  
Flight Control System ◽  
Military Aircraft ◽  
System Operation ◽  
Aircraft Systems ◽  
Manned Flight

Manned flight simulation plays a key role in the design and development of modern aircraft systems where pilot interaction is an important consideration. Examples of the systems simulated during an aircraft project include the flight control system, the head-up display, the weapons system and the warnings system. Flight simulation allows the pilot to assess the system operation at an early stage in the design process, and modifications can be quickly implemented so that optimum system operation can be finalized. At British Aerospace (Military Aircraft Division), Warton, three differently configured simulators are currently utilized in the evaluation of aircraft systems.

scholarly journals New trends in aircraft design

2021 ◽  
Author(s):  
Mária Jabrocká ◽  
◽  
Martin Bugaj
Keyword(s):  
Control System ◽  
Dynamic Stability ◽  
Flight Control ◽  
Aircraft Design ◽  
Hydrogen Fuel ◽  
Flight Control System ◽  
Aircraft Control ◽  
Near Future

Automation, robotic, unconventional arrangement hydrogen are the hallmarks of new trends in aircraft design. The implementation of hydrogen fuel in aircraft appears to be one of the biggest advances in the near future. Automation in aircraft control is based on the reduction of runway requirements. Among the main conclusions of the paper we include the finding that the aircraft does not have to have a classic conventional arrangement of vertical tail surfaces in order to achieve static/dynamic stability of the aircraft. The complexity of the elements of the aircraft stability and flight control system is directly depended on the weight of the aircraft. Upcoming trends in aircraft design should only based on existing concepts.

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