Analysis Model for Design Based on Stiffness Requirement of Direct Drive Electromechanical Actuator |
Oh, Sang Gwan
(Korea Aerospace Research Institute)
Lee, Hee Joong (Korea Aerospace Research Institute) Park, Hyun Jong (Korea Aerospace Research Institute) Oh, Dongho (School of Mechanical Engineering, Chungnam National University) |
1 | Structural Integrations with Control Systems, NASA SP-8079, 1971. |
2 | Lee, H. J., and Kang, E. S., "Development of Direct Drive Electro-mechanical Actuation System for Thrust Vector Control of KSLV-II," Journal of The Korean Society for Aeronautical and Space Sciences, Vol. 44, No. 10, 2016, pp. 911-920. DOI |
3 | Lee, H. J., Kang, E. S., and Song, O. S., "A Study on the Dynamic Characteristics Improvement of Direct Drive Electro-mechanical Actuation System using Dynamic Force Feedback Control," Journal of The Korean Society for Aeronautical and Space Sciences, Vol. 45, No. 4, 2017, pp. 328-341. DOI |
4 | Sun, B. C., Oh, C. S., Park, Y. K., and Roh, W. R., "Thrust Vector Control Stiffness Requirements of Launch Vehicles," Proceeding of The Korean Society for Aeronautical and Space Sciences Fall Conference, November 2012, pp. 2007-2012. |
5 | Renault, C., "Usefulness of A Force Feedback on Electromechanical Actuator," Proceedings of the 6th International ESA Conference on Guidance, Navigation and Control Systems, Vol. 1, 18.1-18.10, 2005. |
6 | Cowan, J. R., and Weir, R. A., "Design and Test of Electromechanical Actuators for Thrust Vector Control," The 27th Aerospace Mechanisms Symposium, 2016, pp. 349-366. |
7 | Bilyaletdinova, L., and Steblinkin, A., "Simulation of Direct Electromechanical Actuator with Ballscrew," Procedia Engineering 176, 2017, pp. 85-95. DOI |
8 | MIL-B-82820F, Military Specification, February 1994. |
9 | Super Precision Bearing Catalogue, NSK Korea, June 2015. |
10 | Roller Screw Catalogue, SKF Group, April 2014. |
11 | Min, B. J., Choi, H. D., and Kang, E. S., "Research of Synthetic Resonance Characteristics for Electrohydraulic Thrust Vector Control Actuation System," Aerospace Engineering and Technology, Vol. 7, No. 1, July 2008, pp. 151-160. |