Citation: | Huang Wei, Chen Zhitong, Chen Wuyi, et al. Principle of machining variant curvature blending surfaces with counter torus cutter[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(8): 1118-1123. (in Chinese) |
[1] |
周济,周艳红.数控加工技术[M].北京:国防工业出版社,2002:46-47 Zhou Ji,Zhou Yanhong.Technology of NC machining[M].Beijing:National Defence Industry Press,2002:46-47(in Chinese)
|
[2] |
Hamakhan I A,Korakianitis T.Aerodynamic performance effects of leading-edge geometry in gas-turbine blades[J].Applied Energy,2010,87(5):1591-1601
|
[3] |
Kim B H,Choi B K.Guide surface based tool path generation in 3-axis milling:an extension of the guide plane method[J].Computer Aided Design,2000,32:191-199
|
[4] |
Lee E.Contour offset approach to spiral tool path generation with constant scallop height[J].Computer Aided Design,2003,35:511-518
|
[5] |
Sun Y W,Guo D M,Jia Z Y.Spiral cutting operation strategy for machining of sculptured surfaces by conformal map approach[J].Journal of Material Process Technology,2006,180:74-82
|
[6] |
Kruth P,Klewais J P.Optimization and dynamic adaptation of the cutter inclination during five-axis milling of sculptured surfaces[J].CIRP Annals,1994,43(1):443-448
|
[7] |
Shan C W,Zhang D H,Liu W W,et al.A novel spiral machining approach for blades modeled with four patches[J].Internal Journal of Advanced Manufacturing Technology,2009,43:563-572
|
[8] |
You C F,Sheen B T,Lin T K.Robust spiral tool-path generation for arbitrary pockets[J].Internal Journal of Advanced Manufacturing Technology,2001,17:181-188
|
[9] |
伊宗М X.燃气涡轮发动机叶片的机械加工[M].北京:国防工业出版社,1965 Yi Zong M X.Machining of gas twrbine engine blades[M].Beijing:Natinal Defence of Industry Press,1965(in Chinese)
|
[10] |
Chiou C J,Lee Y S.A shape-generating approach for multi-axis machining G-buffer models[J].Computer-Aided Design,1999(31):761-776
|
[11] |
Yoon Jounghahn,Pottmann Helmut,Lee Yuanshin.Locally optimal cutting positions for 5-axis sculptured surface machining[J].Computer-Aided Design,2003,35:69-81
|
[12] |
张洪.从增大行距宽度减小波纹度的角度看型面加工发展的方向 .北京:北京航空学院制造工程系,1982 Zhang Hong.Observing the development of machining sculptured surfaces from the perspective of increasing strip width and decreasing waviness .Beijing:Manufacturing Engineering Department,Beijing Institute of Aeronautics,1982(in Chinese)
|
[13] |
吕雪丽,张洪.广域曲率吻合原则与复杂曲面数控加工的全面优化[J].机械设计与制造,2003,10(5):94-96 Lü Xueli,Zhang Hong.Principle of global curvature fitting and global optimization of sculptured surface NC machining[J].Machinery Design and Machining,2003,10(5):94-96(in Chinese)
|
[14] |
Yu Guang.General tool correction for five-axis milling[J].International Journal of Advanced Manufacturing Technology,1995,10(5):374-378
|
[1] | LIU Y S,YANG Y X,LIU Y,et al. Gust alleviation control system of flexible aircraft considering rudder efficiency[J]. Journal of Beijing University of Aeronautics and Astronautics,2025,51(1):248-256 (in Chinese). doi: 10.13700/j.bh.1001-5965.2022.0952. |
[2] | CHEN Qing-yang, XIN Hong-bo, LU Ya-fei, WANG Peng, WANG Yu-jie, ZHENG Jun-fei. Ground Taxiing Lateral Deviation Correction Control for High Subsonic UAVs[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0635 |
[3] | XU Xingguang, YU Jianglong, GUO Hongfei, REN Zhang. Optimization method of winged aircraft configuration and topology for cooperative penetration[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0818 |
[4] | CHANG Jiaming, LI Sulan, DUAN Xuechao, ZHANG Wei, WANG Chenyang. Anti-stochastic disturbance control of airship[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0489 |
[5] | MENG Z P,YANG L Q,WANG B,et al. ADRC design for folding wing vehicles based on improved equilibrium optimization algorithm[J]. Journal of Beijing University of Aeronautics and Astronautics,2024,50(8):2449-2460 (in Chinese). doi: 10.13700/j.bh.1001-5965.2022.0698. |
[6] | NIE Li, LI Chenliang, LIU Wangkui, SHEN Haidong, LIU Yanbin, CHEN Jinbao. Adaptive neural network based fixed-time command-filtered control for quadrotor unmanned aerial vehicles[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0403 |
[7] | HE Hai-yang, ZHAO Zhen-gen, KONG Fei. Longitudinal control of fixed-wing UAV based on deep reinforcement learning[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0075 |
[8] | SU Zi-kang, CHEN Jia, LI Xue-bing, LI Chun-tao. Coordinated Control of Transition Flight Position and Attitude for Quad Tilt-Rotor UAV[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0622 |
[9] | KONG Lingwei, LI Weiqi. Optimization of aircraft speed vector control based on Hp adaptive Pseudo-spectral method[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0405 |
[10] | FENG Yu-xuan, HUO Ying-yuan, LI Jun-jie. Design of multiple-input/multiple-output control law for active flutter suppression of flying-wing aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0144 |
[11] | ZHAO Q,ZHEN Z Y,GONG H J,et al. UAV formation control based on dueling double DQN[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(8):2137-2146 (in Chinese). doi: 10.13700/j.bh.1001-5965.2021.0601. |
[12] | ZHOU B J,YU C Q,TAN L L,et al. Fast leveling control technology of vehicle platform based on interference compensation[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(6):1495-1503 (in Chinese). doi: 10.13700/j.bh.1001-5965.2021.0447. |
[13] | TAN Cao, YU Peng, LI Bo, LU Jia-yu, REN Yun-yun. Pressure Cascade Control of Brake-by-wire Unit Based on Direct Drive Pump-Valve Cooperative[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0216 |
[14] | ZHANG X C,WAN Z Q,YAN D. Optimal active twist control for rotor vibration reduction[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(12):3397-3408 (in Chinese). doi: 10.13700/j.bh.1001-5965.2022.0105. |
[15] | CUI K K,HAN W,LIU Y J,et al. Automatic wave-off control algorithm for carrier aircraft based on DM-DSC[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(4):900-912 (in Chinese). doi: 10.13700/j.bh.1001-5965.2021.0362. |
[16] | XU Meng, LI Yan, GAO Jie, XU Hai, GAO Bing. Design of aircraft anti-skid braking system integrated sliding mode control based on novel convergence law[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.1085 |
[17] | DUAN B,YANG S,LI A J. Design of LPV control law for unmanned helicopter[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(4):879-890 (in Chinese). doi: 10.13700/j.bh.1001-5965.2021.0340. |
[18] | WEI R K,DAI Y T,YANG C,et al. Numerical study of wing gust response alleviation based on camber morphing trailing edge[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(7):1864-1874 (in Chinese). doi: 10.13700/j.bh.1001-5965.2021.0563. |
[19] | PENG Cheng, SUN Liguo, WANG Yanyang, TAN Wenqian, XIAO Feng. Control oriented longitudinal modeling and analysis of pigeon-like flapping-wing aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(12): 2510-2519. doi: 10.13700/j.bh.1001-5965.2021.0130 |
[20] | YANG Lan, AN Chao, XIE Changchuan, YANG Chao. Gust load alleviation analysis based on vortex lattice method in state-space form[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(7): 1200-1209. doi: 10.13700/j.bh.1001-5965.2021.0023 |