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A status report on the development of an electrical test-facility for the SEAS DTC (Systems Engineering for Autonomous Systems, Defence Technology Centre) project ‘ultra-compact intelligent electrical networks’ is presented. The electrical platform has initially been based on a small, aerial, uninhabited autonomous vehicle architecture, which consists of two electrical generators, a DC distribution system, an energy storage device and various electrical loads. The issues that arise when implementing such a test platform are discussed and a suitable design strategy is proposed along with progress to-date.

The simulation of a power system such as the More Electric Aircraft is a complex problem. There are conflicting requirements of the simulation, for example in order to reduce simulation run-times, power ratings that need to be established over long periods of the flight can be calculated using a fairly coarse model, whereas power quality is established over relatively short periods with a detailed model. An important issue is to establish the requirements of the simulation work at an early stage. This paper describes the modelling and simulation strategy adopted for the UK TIMES project, which is looking into the optimisation of the More Electric Aircraft from a system level. Essentially four main requirements of the simulation work have been identified, resulting in four different types of simulation. Each of the simulations is described along with preliminary models and results.

A status report of the modelling and simulation work that is being undertaken as part of the TIMES (Totally Integrated More Electric Systems) project is presented. Dynamic power quality simulations have been used to asses the performance of the electrical system of a EMA based actuation system for an Airbus A330 size aircraft, for both low voltage 115 V, and high voltage 230 V three-phase AC systems. The high voltage system is shown to have benefits in terms of power quality and reduced size and weight of equipment.