Name
Abstract | ||
|---|---|---|
The aim of this paper is to improve the efficiency of a low pressure compressor within a turbojet engine. For this purpose a new feedback controller will be introduced which compares the actual compressor surge margin to a given reference value. Then, this new feedback controller calculates a deviation on the existing nozzle area schedule such that the overall efficiency of the controller is improved at steady state condition. The major contribution of this work consists in a robust control design approach leading to improved robustness properties and reduced calibration efforts for the controllers of future unmanned aircraft propulsion systems. |
Year | DOI | Venue |
|---|---|---|
2013 | 10.1007/s10846-012-9700-y | Journal of Intelligent and Robotic Systems |
Keywords | Field | DocType |
Energy efficient UAV systems,Aircraft engine control,Robust control,Control applications | Control theory,Propulsion,Control theory,Robustness (computer science),Control engineering,Compressor stall,Gas compressor,Engineering,Robust control,Nozzle,Turbojet | Journal |
Volume | Issue | ISSN |
69 | 1-4 | 0921-0296 |
Citations | PageRank | References |
0 | 0.34 | 1 |
Authors | ||
2 | ||
Name | Order | Citations | PageRank |
|---|---|---|---|
| Benedikt Alt | 1 | 15 | 3.25 |
| Elias Hermann | 2 | 0 | 0.34 |