1. Optimization as a support for selection and design of aircraft actuation systems;Andersson;Optimization,1998
2. Simulation of a prototype electrically powered integrated actuator for civil aircraft;Crowder;Proc Inst Mech Eng G-J Aerosp Eng,1997
3. Navarro R. Performance of an electro-hydrostatic actuator on the F-18 systems research aircraft. Washington, D.C.: NASA;1997. Report No.:NASA/TM-97-206224.
4. Dominique VDB. The A380 flight control electrohydro-static actuators, achievements and lessons learnt. 25th International Congress of the Aeronautical Sciences; 2006 Sep 3–8; Hamburg, Germany. 2006. p. 1–8.
5. A methodology for vehicle and mission level comparison of more electric aircraft subsystem solution: application to the flight control actuation system;Chakraborty;Proc Inst Mech Eng G-J Aerosp Eng,2014