| BTT控制系统半实物仿真方案
设计及试验结果分析 |
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| 引用本文： | 魏明英.BTT控制系统半实物仿真方案
设计及试验结果分析[J].现代防御技术,2001,29(3):34-37. |
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| 作者姓名： | 魏明英 |
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| 作者单位： | 中国航天机电集团公司二院二部, |
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| 摘 要： | BTT控制系统半实物仿真试验以BTT试验器为背景，配合BTT控制技术研究可全面验证导弹控制系统设计。给出了半实物仿真试验方案、方法及试验结果分析，试验结果表明BTT控制系统设计满足最小侧滑(近似零侧滑角)倾斜转弯的技术指标要求，半实物仿真试验方法正确。
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| 关 键 词： | 倾斜转弯 半实物仿真 控制系统 |
| 文章编号： | 1009-086X(2001)03-0034-04 |
| 修稿时间： | 2001年1月16日 |
Hardware in the Loop Simulation Scheme and Experimental Results Analysis of BTT
Control System |
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| WEI Ming,ying.Hardware in the Loop Simulation Scheme and Experimental Results Analysis of BTT
Control System[J].Modern Defence Technology,2001,29(3):34-37. |
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| Authors: | WEI Ming ying |
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| Abstract: | Hardware in the loop simulation of BTT control system can completely validate the design result of missile control system based on BTT simulator and directed by the research on BTT control technology. A scheme of hardware in the loop simulation is put forward in this paper. The analysis of experimental results show that the scheme is reasonable and the designed BTT control system can meet the technological guideline of achieving bank to turn with the minimum (almost zero) sideslip angle. |
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| Keywords: | Bank-to turn(BTT) Hardware in the loop simulation (Semi physical simulation) Control system |
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