Information fusion estimation–based flight control of a nonlinear jumbo jet under wind disturbance

Zhen Ziyang; Xu Yue; Jiang Ju

摘要

Summary >Wind disturbance has a large impact on the safety and comfort of jumbo jets. An information fusion estimation–based control method, which is based on the linearization‐based design strategy, is proposed for the flight control of a nonlinear jumbo jet to restrain wind disturbance. A complete nonlinear model of the jumbo jet is developed based on the aerodynamic data and parameters of a Boeing jumbo jet. An information fusion control (IFC) scheme based on information fusion estimation is presented for the nonzero‐state tracking problem of the linear system with disturbance. The IFC scheme fuses the information of desired future states, desired control inputs, system dynamic equations, and performance index function. IFC is applied in the automatic flight control system of the jumbo jet to design the longitudinal flight controller and lateral flight controller. Simulation results show the feasibility and effectiveness of the IFC in the flight control of the jumbo jet, as compared with the PID control and the traditional linear quadratic optimal control. </abstract> </span> <span class="z_kbtn z_kbtnclass hoverxs" style="display: none;">展开▼</span> </div> <div class="translation abstracttxt"> <span class="zhankaihshouqi fivelineshidden" id="abstract"> <span>机译：</span><Abstract XMLNS =“http://www.wiley.com/namespaces/wiley”type =“main”xml：lang =“en”xml：id =“oca2357-abs-abs-0001”> <标题类型=“main” >摘要</标题> >风扰动对巨型喷气机的安全性和舒适性产生了很大影响。基于基于线性化的设计策略的基于信息融合估计的控制方法，提出了一种非线性巨型射流的飞行控制，以抑制风扰动。基于波音巨头喷射器的空气动力学数据和参数，开发了一种简化的巨型射流的非线性模型。介绍了基于信息融合估计的信息融合控制（IFC）方案用于干扰的线性系统的非零状态跟踪问题。 IFC方案融合了所需的未来状态，期望的控制输入，系统动态方程和性能索引功能的信息。 IFC应用于Jumbo Jet的自动飞行控制系统，以设计纵向飞行控制器和横向飞行控制器。仿真结果表明，与PID控制和传统的线性二次最佳控制相比，巨型射流飞行控制中IFC的可行性和有效性。</ p> </摘要> </span> <span class="z_kbtn z_kbtnclass hoverxs" style="display: none;">展开▼</span> </div> </div> <div class="record"> <h2 class="all_title" id="enpatent33" >著录项</h2> <ul> <li> <span class="lefttit">来源</span> <div style="width: 86%;vertical-align: text-top;display: inline-block;"> <a href='/journal-foreign-27675/'>《Optimal Control Applications and Methods》</a> <b style="margin: 0 2px;">|</b><span>2018年第2期</span><b style="margin: 0 2px;">|</b><span>共12页</span> </div> </li> <li> <div class="author"> <span class="lefttit">作者</span> <p id="fAuthorthree" class="threelineshidden zhankaihshouqi"> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Zhen Ziyang&option=202" target="_blank" rel="nofollow">Zhen Ziyang;</a> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Xu Yue&option=202" target="_blank" rel="nofollow">Xu Yue;</a> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Jiang Ju&option=202" target="_blank" rel="nofollow">Jiang Ju;</a> </p> <span class="z_kbtnclass z_kbtnclassall hoverxs" id="zkzz" style="display: none;">展开▼</span> </div> </li> <li> <div style="display: flex;"> <span class="lefttit">作者单位</span> <div style="position: relative;margin-left: 3px;max-width: 639px;"> <div class="threelineshidden zhankaihshouqi" id="fOrgthree"> <p>College of Automation EngineeringNanjing University of Aeronautics and AstronauticsNanjing 211106 China;</p> <p>College of Automation EngineeringNanjing University of Aeronautics and AstronauticsNanjing 211106 China;</p> <p>College of Automation EngineeringNanjing University of Aeronautics and AstronauticsNanjing 211106 China;</p> </div> <span class="z_kbtnclass z_kbtnclassall hoverxs" id="zhdw" style="display: none;">展开▼</span> </div> </div> </li> <li > <span class="lefttit">收录信息</span> <span style="width: 86%;vertical-align: text-top;display: inline-block;"></span> </li> <li> <span class="lefttit">原文格式</span> <span>PDF</span> </li> <li> <span class="lefttit">正文语种</span> <span>eng</span> </li> <li> <span class="lefttit">中图分类</span> <span><a href="https://www.zhangqiaokeyan.com/clc/1147.html" title="应用数学">应用数学;</a></span> </li> <li class="antistop"> <span class="lefttit">关键词</span> <p style="width: 86%;vertical-align: text-top;"> <a style="color: #3E7FEB;" href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=automatic flight control system&option=203" rel="nofollow">automatic flight control system;</a> <a style="color: #3E7FEB;" href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=information fusion&option=203" rel="nofollow">information fusion;</a> <a style="color: #3E7FEB;" href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=jumbo jet&option=203" rel="nofollow">jumbo jet;</a> <a style="color: #3E7FEB;" href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=linear quadratic optimal control&option=203" rel="nofollow">linear quadratic optimal control;</a> </p> <div class="translation"> 机译：自动飞行控制系统;信息融合;Jumbo Jet;线性二次最优控制; </div> </li> </ul> </div> </div> <div class="literature cardcommon"> <div class="similarity "> <h3 class="all_title" id="enpatent66">相似文献</h3> <div 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FANG Zheng</a> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=房正&option=202" target="_blank" rel="nofollow" class="tuijian_auth tuijian_authcolor">,房正</a> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=LI Xiao-wei&option=202" target="_blank" rel="nofollow" class="tuijian_auth tuijian_authcolor">,LI Xiao-wei</a> <span> <a href="/conference-cn-60216/" target="_blank" rel="nofollow" class="tuijian_authcolor"> . 第十三届全国水动力学学术会议暨第二十六届全国水动力学研讨会 </a> <span> <span> . 2014</span> </span> </div> </li> <li> <div> <b>7. </b><a class="enjiyixqcontent" href="/academic-degree-domestic_mphd_thesis/020313002848.html">飞翼飞行平台强扰动下的飞行边界控制技术</a> <b>[A] </b> <span> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=孔琳玲&option=202" target="_blank" rel="nofollow" class="tuijian_auth tuijian_authcolor"> . 孔琳玲</a> <span> . 2009</span> </span> </div> </li> </ul> <ul style="display: none;"> <li> <div> <b>1. </b><a class="enjiyixqcontent" href="/patent-detail/06120113999123.html">基于飞行数据的扰动风定制化建模和大气数据估计方法</a> <b>[P]</b> . <span> 中国专利： CN114091180A </span> <span> . 2022-02-25</span> </div> </li> <li> <div> <b>2. </b><a class="enjiyixqcontent" href="/patent-detail/06120113066308.html">一种基于飞行数据的大气数据和扰动风估计方法</a> <b>[P]</b> . <span> 中国专利： CN113111597A </span> <span> . 2021-07-13</span> </div> </li> <li> <div> <b>3. </b><a class="enjiyixqcontent" href="/patent-detail/06130407813541.html">DISTURBANCE ACCELERATION SPEED ESTIMATION METHOD, HULL AUTOMATIC CONTROL METHOD, DISTURBANCE ACCELERATION SPEED ESTIMATION DEVICE, AND DISTURBANCE ACCELERATION SPEED ESTIMATION COMPUTER PROGRAM</a> <b>[P]</b> . <span> 外国专利：  JP2018125012A </span> <span> . 2018-08-09</span> </div> <p class="zwjiyix translation" style="max-width: initial;height: auto;word-break: break-all;white-space: initial;text-overflow: initial;overflow: initial;"> <span>机译：扰动加速速度估计方法，船体自动控制方法，扰动加速速度估计装置和扰动加速速度估计计算机程序 </span> </p> </li> <li> <div> <b>4. </b><a class="enjiyixqcontent" href="/patent-detail/06130407755203.html">Disturbance acceleration estimation method, hull automatic control method, disturbance acceleration estimation device, and disturbance acceleration estimation computer program</a> <b>[P]</b> . <span> 外国专利：  JP6372046B2 </span> <span> . 2018-08-15</span> </div> <p class="zwjiyix translation" style="max-width: initial;height: auto;word-break: break-all;white-space: initial;text-overflow: initial;overflow: initial;"> <span>机译：扰动加速度估计方法，船体自动控制方法，扰动加速度估计装置和扰动加速度估计计算机程序 </span> </p> </li> <li> <div> <b>5. </b><a class="enjiyixqcontent" href="/patent-detail/06130403179586.html">Control Apparatus using approximation-based disturbance observer approach for adaptive tracking of uncertain pure-feedback nonlinear systems with unmatched disturbances</a> <b>[P]</b> . <span> 外国专利：  KR101966155B1 </span> <span> . 2019-04-08</span> </div> <p class="zwjiyix translation" style="max-width: initial;height: auto;word-break: 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