| STUDIES ON AIRCRAFT TOTAL ENERGY FLIGHT CONTROL SYSTEM：NONLINEAR SYSTEM INTEGRATION AND SIMULATION |
| |
| 作者姓名： | Wu Shufan Shen Yongzhang Guo Suofeng |
| |
| 作者单位： | Dept of Automatic Control，Nanjing University of Aeronauticsand Asironautics，Nanjing，China，210016 |
| |
| 摘 要： | ＳＴＵＤＩＥＳＯＮＡＩＲＣＲＡＦＴＴＯＴＡＬＥＮＥＲＧＹＦＬＩＧＨＴＣＯＮＴＲＯＬＳＹＳＴＥＭ：ＮＯＮＬＩＮＥＡＲＳＹＳＴＥＭＩＮＴＥＧＲＡＴＩＯＮＡＮＤＳＩＭＵＬＡＴＩＯＮＷｕＳｈｕｆａｎ；ＳｈｅｎＹｏｎｇｚｈａｎｇ；ＧｕｏＳｕｏｆｅｎｇ（Ｄｅｐｔ...
|
STUDIES ON AIRCRAFT TOTAL ENERGYFLIGHT CONTROL SYSTEM: NONLINEARSYSTEM INTEGRATION AND SIMULATION |
| |
| Wu Shufan, Shen Yongzhang, Guo Suofeng.STUDIES ON AIRCRAFT TOTAL ENERGYFLIGHT CONTROL SYSTEM: NONLINEARSYSTEM INTEGRATION AND SIMULATION[J].Chinese Journal of Aeronautics,1995(1). |
| |
| Authors: | Wu Shufan Shen Yongzhang Guo Suofeng |
| |
| Abstract: | Based on the designed results for the linear part of total energy flight con-trol system, this paper further studies various nonlinear flight altitude and speed controlmodes. The linear altitude and speed control loops are first analyzed and designed. Va-rious nonlinear operational hmitations are then discussed and implemented in the sys-tem. The energystate dynamics of aireraft under limited thrust are analyzed, and con-trol pnorities on flight speed or path are implemented through processing appropriatelythe normalized command signals. Fnially, digital simulations of this nonlinearmulti-variable control system are conductcd with a Boeing-707 transport aircraft mod-el. and satisfactory system performance is evaluated. |
| |
| Keywords: | flight control thrust control nonlinearity simulation |
| 本文献已被 CNKI 等数据库收录！ |
