碩士 / 國立臺北科技大學 / 自動化科技研究所 / 107 / The paper proposes a synchronous flight control system to design a force feedback control system to simulate the reaction force of the joystick in different attitude control, and to realize the irreversible force sense for both pilot and co-pilot. The system separately uses the flight force model and force feedback controller designed strategy. The force model is based on two-mass mechanical systems to simulate the real manipulator (non-linear force and position) of the aircraft. The force measurement equipment is further used to obtain the real system position-force characteristic curve in order to establish the force model. The force feedback controller uses the impedance theory to simulate the characteristic of the created two mass-damping spring system, and achieves the force control in different position, presenting the real dynamic force feedback characteristic. The system and design proposed in this paper can be applied to the construction of dynamic simulation systems for different aircrafts.
| Identifer | oai:union.ndltd.org:TW/107TIT00146011 |
| Date | January 2019 |
| Creators | CHANG, CHE-WEI, 張哲瑋 |
| Contributors | CHEN, CHIN-SHENG, 陳金聖 |
| Source Sets | National Digital Library of Theses and Dissertations in Taiwan |
| Language | zh-TW |
| Detected Language | English |
| Type | 學位論文 ; thesis |
| Format | 58 |
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