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Future architecture of flight control systems
IEEE Aerospace and Electronic Systems Magazine, 2002The development of fault tolerant embedded control systems such as flight control systems (FCS) are currently highly specialized and time-consuming. We introduce a conceptual architecture for the next decade control system where all control and logic are distributed to a number of computer nodes locally linked to actuators and connected via a ...
K. Alstrom, J. Torin
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Aircraft Controller Flight Control System Design
Applied Mechanics and Materials, 2014The servo control methods of motion configuration are researched. Based on analysis for characteristic of the motion configuration, the control strategy and control law used on the motion control system are presented. The controllers are respectively designed by frequency correcting method and normal control method which belongs to classical control ...
Hong Cheng Zhou, Dao Bao Wang
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Flight control system of Hypersonic Flight Experiment vehicle
21st Atmospheric Flight Mechanics Conference, 1996This paper describes the flight control system of the Hypersonic Flight Experiment vehicle. The experiment was conducted in early 1996. This paper summarizes the vehicle, sensor, on-board computer, control effectors, navigation, guidance, and control laws. In addition, the actual flight is compared with a simulated flight. The obtained flight data show
Shinji Ishimoto +3 more
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Aircraft flight control systems
The Aeronautical Journal, 1999AbstractThis paper presents a short account of the flight control systems used in commercial transport, military combat and general aviation aircraft. The effects of aircraft safety, reliability and weather delays on satisfactory aircraft operations are shown to be significant reasons for the extensive use of flight control systems.
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SAE Technical Paper Series, 1997
<div class="htmlview paragraph">The Fly-By-Light Advanced Systems Hardware (FLASH) program developed Fly-By-Light (FBL) and Power-By-Wire (PBW) technologies for military and commercial aircraft. FLASH consisted of three tasks. Task 1 developed the fiber optic cable, connectors, testers and installation and maintenance procedures. Task 3 developed
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<div class="htmlview paragraph">The Fly-By-Light Advanced Systems Hardware (FLASH) program developed Fly-By-Light (FBL) and Power-By-Wire (PBW) technologies for military and commercial aircraft. FLASH consisted of three tasks. Task 1 developed the fiber optic cable, connectors, testers and installation and maintenance procedures. Task 3 developed
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Self-Repairing Flight Control System
SAE Technical Paper Series, 1984<div class="htmlview paragraph">This paper describes a technique for flight control system reconfiguration following a control surface failure. The methodology involves the reallocation of flight control commands to the surviving control surfaces following a failure. The algorithms developed are aimed at reconfiguration without pilot intervention
R.R. Huber, B. McCulloch
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[1992] Proceedings IEEE/AIAA 11th Digital Avionics Systems Conference, 2003
The authors describe the C-17 flight control system (FCS), starting with the aircraft requirements for deep stall avoidance, probability of loss of control, all engine out control, and safe go-around requirements. FCS requirements derived from the aircraft requirements are described.
B.W. Kowal, C.J. Scherz, R. Quinlivan
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The authors describe the C-17 flight control system (FCS), starting with the aircraft requirements for deep stall avoidance, probability of loss of control, all engine out control, and safe go-around requirements. FCS requirements derived from the aircraft requirements are described.
B.W. Kowal, C.J. Scherz, R. Quinlivan
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Robust Flight Control System Design
IFAC Proceedings Volumes, 1981Abstract The short period longitudinal mode of an F4-E aircraft with additional horizontal canards is unstable in subsonic flight and unsufficiently damped at supersonic speed. The control system has to provide acceptable pole locations according to military specifications for flying qualities.
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SAE Technical Paper Series, 1967
<div class="htmlview paragraph">The C-5A flight control system is explained with individual schematics illustrating each subsystem. Several mechanical failure situations and necessary pilot actions are described. The distribution of hydraulic power and its importance on an airplane which uses fully powered hydraulic flight controls is explained ...
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<div class="htmlview paragraph">The C-5A flight control system is explained with individual schematics illustrating each subsystem. Several mechanical failure situations and necessary pilot actions are described. The distribution of hydraulic power and its importance on an airplane which uses fully powered hydraulic flight controls is explained ...
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Part Three—Flight Control System
Aircraft Engineering and Aerospace Technology, 1962AT the present day the operations of civil transport aeroplanes are severely restricted under conditions of poor visibility and not infrequently flights have to be diverted or cancelled. The work of the Blind Landing Experimental Unit of the Ministry of Aviation in the development of a system of automatic landing for military aircraft has been ...
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