System Modeling, Simulation, and Analysis of Electrohydrostatic Actuator for Armoured Recovery Vehicles

Author:

Kumar Manish,Singh Shweta

Publisher

Springer Singapore

Reference23 articles.

1. Alle N, Hiremath SS, Makaram S, Subramaniam K, Talukdar A (2016) Review on electro hydrostatic actuator for flight control. Int J Fluid Power 2332–2343

2. Alden R (1991) Power-by-wire flight control systems. In: Proceedings of the IEEE conference on national aerospace and electronics NAECON, vol 2, pp 535–539

3. Botten SL, Whitley CR (2000) Flight control actuation technology for next-generation all electric aircraft. Technol Rev J Millennium Issue 23(6):55–68

4. Rongjie K, Zongxia J, Shaoping W, Lisha C (2009) Design and simulation of electro-hydrostatic actuator with a built-in power regulator. Chin J Aeronaut 700–706

5. Park B, Kim TS, Ryu J-S, Hyun DS (2006) Fault tolerant strategies for BLDC motor drives under switch faults. In: Proceedings of the conference on industry applications

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