电光与控制, 2010, 17 (5): 74, 网络出版: 2010-06-22  

动态条件下进近着陆系统引导误差计算与补偿

Calculation and Compensation of Guidance Error for Approach and Landing System in Dynamic Condition
作者单位
1 空军工程大学 电讯工程学院,西安 710077
2 上海航电公司军事代表室,上海 200233
摘要
平台运动将导致着陆引导信息出现偏差,为准确分析和计算动态平台条件下进近着陆系统着陆引导误差变化,提出了一种基于动态坐标转换对引导误差进行计算与补偿的方法。该方法依据GPS测姿中动态坐标转换原理,将平台运动分解为偏航、横滚、俯仰和升降4种姿态,建立了动态平台上进近着陆系统引导误差的数学模型,利用该模型对平台各摇摆处于简谐运动条件引导误差进行了仿真分析,依此设计了引导误差补偿的方案框图。该方法可以实现平台运动条件下对引导误差的仿真计算,能够对引导误差进行实时补偿。
Abstract
The movement of platform may cause error in landing guidance information. In order to correctly analyze and calculate the guidance error of the approach and landing system under dynamic condition, a new method is presented based on dynamic coordinate conversion. According to the principle of the dynamic coordinate conversion from the attitude measurement of the GPS theory, a mathematic model of the guidance error of the approach and landing system onboard the platform was built up, where the dynamic status of the platform was decomposed into four statuses: yaw, roll, pitch and elevation. Then the model was used in simulation and calculation of the guidance error when the platform was in simple harmonic motion, based on which a scheme for compensation of the guidance error was proposed. Simulation results indicated that the coordinate conversion can be used for simulation of the guidance parameter error in the dynamic condition, and also for compensating the error in real time.

戴传金, 吴德伟, 赵修斌, 陈校平, 王巍. 动态条件下进近着陆系统引导误差计算与补偿[J]. 电光与控制, 2010, 17(5): 74. DAI Chuanjin, WU Dewei, ZHAO Xiubin, CHEN Xiaoping, WANG Wei. Calculation and Compensation of Guidance Error for Approach and Landing System in Dynamic Condition[J]. Electronics Optics & Control, 2010, 17(5): 74.

关于本站 Cookie 的使用提示

中国光学期刊网使用基于 cookie 的技术来更好地为您提供各项服务,点击此处了解我们的隐私策略。 如您需继续使用本网站,请您授权我们使用本地 cookie 来保存部分信息。
全站搜索
您最值得信赖的光电行业旗舰网络服务平台!