1. Crowder, R. and Maxwell, C., “Simulation of a Prototype Electrically Powered Integrated Actuator for Civil Aircraft,” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Vol. 211, No. 6, pp. 381–394, 1997.
2. Van Den Bossche, D., “The A380 Flight Control Electrohydrostatic Actuators, Achievements and Lessons Learnt,” Proc. of 25th International Congress of the Aeronautical Sciences, pp. 1–8 2006.
3. Navarro, R., “Performance of an Electro-Hydrostatic Actuator on the F-18 Systems Research Aircraft,” NASA Technical Reports Server, Document ID: 19970034702, 1997.
4. Chakraborty, I., Mavris, D. N., Emeneth, M., and Schneegans, A., “A Methodology for Vehicle and Mission Level Comparison of More Electric Aircraft Subsystem Solutions: Application to the Flight Control Actuation System,” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Vol. 229, No. 6, pp. 1088–1102, 2015.
5. Crowder, R. M., “Electrically Powered Actuation for Civil Aircraft,” Proc. of IEE Colloquium on Actuator Technology: Current Practice and New Developments, 1996.