DLR develops custom flight control system for SHEFEX II

The German Aerospace Center (Deutsches Zentrum für Luft- und Raumfahrt; DLR) has developed a custom aerodynamic flight control system for SHEFEX II, which will be used to control the craft as it returns to Earth.

At the heart of the canard control system, developed by researchers at the DLR Institute of Flight Systems in Braunschweig, are control surfaces – the canards – on the front section of the research vehicle, which can be used to actively control the vehicle. Initial ground tests were successful; now the sub-module is ready for integration into SHEFEX II and further testing.

"Electromechanical flight control systems have great potential for future re-entry vehicles," says DLR flight systems engineer Andreas Koch of the background to the experiment. "The prototype developed by DLR is very compact and light. It is a step towards cheaper and more efficient flight control systems for re-entry vehicles," the researcher states.

The canard control system can automatically adjust the position and flow conditions of the re-entry vehicle – in the same way that the control surfaces on a plane can be angled to change its attitude. However, the conditions at altitudes of 100–20 kilometres – where the steering fin system is active – are quite different. "We are at the limits of technical feasibility here," explains Koch, adding: "We are flying and taking measurements in the thermosphere, mesosphere and stratosphere. Above 100 kilometres, there is not an absolute vacuum, but the air there is so thin that aerodynamic forces cannot affect the attitude of the vehicle."

The new steering fin system is exposed to extreme aerodynamic and thermal loads. The components must withstand heat, large accelerations and high aerodynamic loads. These would cause standard components to break apart and burn up.

Re-entry systems are amongst the most advanced technologies. They have to function reliably in a very inhospitable environment. SHEFEX II will reach speeds of almost three kilometres per second during re-entry – a speed at which you could get from New York to Washington DC in 130 seconds. The canard module – that is, the hardware – therefore has to be sufficiently robust to withstand such extreme conditions. Yet at the same time, it needs software on board that can work reliably throughout the demanding experimental mission, and bring the vehicle back to Earth in a controlled manner.

FLUG REVUE 07/2018


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