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Realization of nonlinear PID with feed-forward controller for 3-DOF flight simulator and hardware-in-the-loop simulation 被引量:3
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作者 Duan Haibin Wang Daobo Yu Xiufen 《Journal of Systems Engineering and Electronics》 SCIE EI CSCD 2008年第2期342-345,共4页
As friction, intrinsic steady-state nonlinearity poses a challenging dilemma to the control system of 3-DOF (three degree of freedom) flight simulator, a novel hybrid control strategy of nonlinear PID (proportional... As friction, intrinsic steady-state nonlinearity poses a challenging dilemma to the control system of 3-DOF (three degree of freedom) flight simulator, a novel hybrid control strategy of nonlinear PID (proportionalintegral-derivative) with additional FFC (feed-forward controller) is proposed, and the hardware-in-the-loop simulation results are also given. Based on the description of 3-DOF flight simulator, a novel nonlinear PID theory is well introduced. Then a nonlinear PID controller with additional FFC is designed. Subsequently, the loop structure of 3-DOF flight simulator is also designed. Finally, a series of hardware-in-the-loop simulation experiments are undertaken to verify the feasibility and effectiveness of the proposed nonlinear PID controller with additional FFC for 3-DOF flight simulator. 展开更多
关键词 flight simulator nonlinear PID FFC hardware-in-the-loop.
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RflySim ToolChain:a rapid development and validation toolchain for intelligent unmanned swarm systems
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作者 DAI Xunhua TU Jinhu QUAN Quan 《Journal of Systems Engineering and Electronics》 2025年第4期1077-1093,共17页
Developing intelligent unmanned swarm systems(IUSSs)is a highly intricate process.Although current simulators and toolchains have made a notable contribution to the develop-ment of algorithms for IUSSs,they tend to co... Developing intelligent unmanned swarm systems(IUSSs)is a highly intricate process.Although current simulators and toolchains have made a notable contribution to the develop-ment of algorithms for IUSSs,they tend to concentrate on iso-lated technical elements and are deficient in addressing the full spectrum of critical technologies and development needs in a systematic and integrative manner.Furthermore,the current suite of tools has not adequately addressed the challenge of bridging the gap between simulation and real-world deployment of algorithms.Therefore,a comprehensive solution must be developed that encompasses the entire IUSS development life-cycle.In this study,we present the RflySim ToolChain,which has been developed with the specific aim of facilitating the rapid development and validation of IUSSs.The RflySim ToolChain employs a model-based design(MBD)approach,integrating a modeling and simulation module,a lower reliable control mo-dule,and an upper swarm decision-making module.This compre-hensive integration encompasses the entire process,from mo-deling and simulation to testing and deployment,thereby enabling users to rapidly construct and validate IUSSs.The prin-cipal advantages of the RflySim ToolChain are as follows:it pro-vides a comprehensive solution that meets the full-stack devel-opment needs of IUSSs;the highly modular architecture and comprehensive software development kit(SDK)facilitate the automation of the entire IUSS development process.Further-more,the high-fidelity model design and reliable architecture solution ensure a seamless transition from simulation to real-world deployment,which is known as the simulation to reality(Sim2Real)process.This paper presents a series of case stu-dies that illustrate the effectiveness of the RflySim ToolChain in supporting the research and application of IUSSs. 展开更多
关键词 simulation unmanned aerial vehicle(UAV) SWARM RflySim hardware-in-the-loop(HIL) model-based design(MBD)
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激光制导武器半实物仿真系统的设计与实现 被引量:22
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作者 范世鹏 林德福 +1 位作者 路宇龙 宗睿 《红外与激光工程》 EI CSCD 北大核心 2014年第2期394-397,共4页
首先,以某激光制导弹药为背景,提出了室内半实物仿真系统的总体设计方案,介绍了一种激光半主动导引头的工作原理。其次,在室内局限环境下,建立了弹目几何关系的数学模型,研究了导引头入瞳光学特性,并根据制导与控制系统的工作原理,设计... 首先,以某激光制导弹药为背景,提出了室内半实物仿真系统的总体设计方案,介绍了一种激光半主动导引头的工作原理。其次,在室内局限环境下,建立了弹目几何关系的数学模型,研究了导引头入瞳光学特性,并根据制导与控制系统的工作原理,设计了末制导段弹道的半实物仿真模型。最后,设置两种末端制导的初始条件,引入导引头和角速率陀螺等弹上部件进行多次弹道仿真试验。试验结果表明,基于该导引头和角速率陀螺的制导与控制系统设计合理,可以实现精确打击。 展开更多
关键词 半实物仿真 末制导武器 激光半主动导引头 光学特性 hardware-in-the-loop simulation(HILS)
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Windows平台下的实时仿真计算机系统PCRTSim 被引量:4
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作者 李兴玮 张卫华 黄柯棣 《计算机工程与设计》 CSCD 2004年第5期727-730,共4页
普通微型计算机由于各种相互兼容的标准硬件及丰富的应用软件支持而获得了广泛的应用,但它们之上往往都是运行多任务、多用户的Windows操作系统,一般不能满足半实物仿真的实时性要求。详细介绍了一个Windows平台下的实时仿真计算机系统P... 普通微型计算机由于各种相互兼容的标准硬件及丰富的应用软件支持而获得了广泛的应用,但它们之上往往都是运行多任务、多用户的Windows操作系统,一般不能满足半实物仿真的实时性要求。详细介绍了一个Windows平台下的实时仿真计算机系统PCRTSim,重点研究了PCRTSim下的实时时钟获取问题、帧时间不稳定问题,提出了保证实时仿真帧时间的具体思路,并通过一个简单例子探讨了PCRTSim的具体应用。 展开更多
关键词 WINDOWS平台 实时仿真 计算机系统 PCRTSim 半实物仿真 帧时间
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仿真计算机和仿真软件发展 被引量:1
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作者 桂先洲 黄柯棣 戴金海 《国防科技大学学报》 EI CAS CSCD 北大核心 1994年第4期53-57,共5页
介绍仿真机和仿真软件的发展,分析了银河仿真机系统性能,探讨了仿真机的未来发展特征。
关键词 仿真机 结构 仿真环境 仿真软件 系统仿真
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半实物仿真惯组输出模拟及转台姿态补偿方法 被引量:1
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作者 周国峰 陈喆 +2 位作者 吕瑞 涂海峰 徐珊 《系统工程与电子技术》 EI CSCD 北大核心 2022年第4期1329-1335,共7页
针对半实物仿真传统三轴转台解耦方法大多不考虑地球自转影响造成仿真相似性不足、精度不高的问题,本文充分考虑转台纬度、方位及转序与发射点状态的差异,提出一种虚拟惯组输出模拟及实物惯组转台姿态补偿方法。当设备中不含实物惯组时... 针对半实物仿真传统三轴转台解耦方法大多不考虑地球自转影响造成仿真相似性不足、精度不高的问题,本文充分考虑转台纬度、方位及转序与发射点状态的差异,提出一种虚拟惯组输出模拟及实物惯组转台姿态补偿方法。当设备中不含实物惯组时,通过构建虚拟惯组并考虑误差影响模拟真实惯组输出;当引入实物惯组时,在转台解耦的基础上补偿当地地球自转角速度,根据转台奇异值与仿真需用范围可选卧式或立式驱动模式。经仿真验证,13 min飞行工况下虚拟惯组与实物惯组姿态结果一致,最大角误差约0.08°,不加地速补偿时仿真姿态相比理论值差异约3°,加入补偿后修正至约0.01°,表明该方法正确可行,能有效提高仿真精度,且方法实现简单适用性好,可工程应用并推广。 展开更多
关键词 半实物仿真 惯组模拟 误差与补偿 转台解耦 转台姿态补偿
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