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A method of designing the controller to solve the robust servomechanism problem is applied in the case of an electrohydraulic servo actuating primary flight control. This method is based on the well‐known solution consisting of two separate devices: a servocompensator, in fact an internal model...
Looks at recent developments in methods of decentralising an aircraft’s hydraulic system made possible by the production of miniaturised electro‐hydraulic pumps with their own “smart” actuators.
Integrated modular avionics (IMA) aims to provide highly flexible, reliable and integrated solutions for future aircraft systems which can readily exploit new advances in processor and networking technologies. In this paper, we discuss the problems involved in the provision of appropriate...
This paper discusses the year 2000 problem. After briefly introducing why there is a problem the paper investigates its origins and consequences. Key to resolving the problem of compliance is the need to define what compliance means; this issue is touched on. Attention is then given to the...
Gives an account of the notable features and the author’s view of the main advantages of the V2500 turbofan engine from International Aero Engines.
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