Abstract
Some existing power-by-wire (PBW) airborne actuation systems, such as integrated actuation package, electro-mechanical actuator and electro-hydrostatic actuator, were summarized. The two kinds of the new PBW actuation system, i.e. the electromotor-pump compound control and the electromotor-pump-valve compound control, were proposed. The preliminary experimental analysis have demonstrated that the two new kinds of PBW actuation system, as transition toward all-electric actuation systems, are feasible.
| Original language | English |
|---|---|
| Pages (from-to) | 426-430 |
| Number of pages | 5 |
| Journal | Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics |
| Volume | 25 |
| Issue number | 4 |
| State | Published - Aug 1999 |
| Externally published | Yes |
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