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基于JSBSim的通用空中目标机动仿真模型设计及实现 被引量:1
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作者 郭亚军 丁华 +1 位作者 杨登泰 周兴栋 《航空兵器》 CSCD 北大核心 2021年第3期77-82,共6页
为解决空空导弹试验鉴定数字仿真中目标模型机动样式少、可扩展性差的问题,本文开展了六自由度空中目标机动仿真模型的设计和实现。设计了不同目标机动方式下的法向过载、切向过载、滚转角过载控制律模型;设计了从三个通道过载解算飞机... 为解决空空导弹试验鉴定数字仿真中目标模型机动样式少、可扩展性差的问题,本文开展了六自由度空中目标机动仿真模型的设计和实现。设计了不同目标机动方式下的法向过载、切向过载、滚转角过载控制律模型;设计了从三个通道过载解算飞机升降舵、副翼及油门杆操纵指令之间关系的控制模型;基于开源、开放的飞行动力学模型框架JSBSim开展目标机动仿真模型的实现。研究的仿真模型应用于某型空空导弹鉴定的全数字仿真试验中,比对结果表明,目标模型的仿真机动轨迹与预期机动样式及机动参数较为吻合。 展开更多
关键词 空中目标 机动仿真模型 控制律 JSBSim 试验鉴定
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民用飞机校验机动仿真研究 被引量:3
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作者 刘毅 《民用飞机设计与研究》 2017年第3期54-57,共4页
校验机动是民用飞机纵向俯仰机动中的一种,它是机翼、平尾等部件的载荷严重情况之一。对于校验机动的分析国内国际上的主流是采用机动仿真法。美国的FAR和欧洲的CS适航条款对校验机动有着不同的要求,FAR指定了俯仰角加速的要求,没有指... 校验机动是民用飞机纵向俯仰机动中的一种,它是机翼、平尾等部件的载荷严重情况之一。对于校验机动的分析国内国际上的主流是采用机动仿真法。美国的FAR和欧洲的CS适航条款对校验机动有着不同的要求,FAR指定了俯仰角加速的要求,没有指定俯仰操纵器件的输入;而CS则指定了俯仰操纵器件的输入,对俯仰角加速度没有要求。以往国内校验机动一直以FAR条款为设计基础,对于CS条款的研究和分析不多,以欧洲CS条款为基础,对校验机动的仿真分析进行了研究。 展开更多
关键词 民用飞机 校验机动 机动仿真
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民用飞机控制律对俯仰机动平尾载荷影响分析 被引量:4
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作者 阮文斌 闫中午 符梁栋 《民用飞机设计与研究》 2020年第3期12-16,共5页
针对中国民用航空规章第25部25.331(c)条规定的两种俯仰机动情况(非校验机动和校验机动),本文首先对两种俯仰机动条款进行理解,然后对比分析了中国民用航空规章第25部与欧洲的适航认证规范对校验机动情况存在的差异,最后对两种俯仰机动... 针对中国民用航空规章第25部25.331(c)条规定的两种俯仰机动情况(非校验机动和校验机动),本文首先对两种俯仰机动条款进行理解,然后对比分析了中国民用航空规章第25部与欧洲的适航认证规范对校验机动情况存在的差异,最后对两种俯仰机动考虑控制律前后分别进行机动仿真计算,进而对飞机响应及平尾载荷计算结果进行对比分析。计算分析结果表明:1)考虑控制律后,飞机舵面偏度变化较大,进而导致整个机动过程中飞机响应姿态以及最后的机动载荷变化较大;2)对于急剧移动操作器件的非校验机动,考虑控制律后飞机的响应姿态有所缓减,最后导致平尾载荷有所降低;3)对于相对缓慢移动操作器件的校验机动,考虑控制律后飞机的响应更为剧烈,最后导致平尾载荷有所增加。 展开更多
关键词 俯仰机动 控制律 平尾载荷 机动仿真
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民用飞机控制律对偏航机动载荷影响分析 被引量:3
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作者 阮文斌 张智 《航空工程进展》 CSCD 2020年第6期900-906,共7页
飞机机动过程中方向舵快速大幅偏转会使方向舵和垂尾上产生较大气动载荷并传递到后机身,导致驾驶员来回往复蹬舵造成安全事故。针对CCAR-25部25.351条规定的偏航机动情况及CS-25部25.353规定的偏航机动新条款——方向舵往复偏转,本文首... 飞机机动过程中方向舵快速大幅偏转会使方向舵和垂尾上产生较大气动载荷并传递到后机身,导致驾驶员来回往复蹬舵造成安全事故。针对CCAR-25部25.351条规定的偏航机动情况及CS-25部25.353规定的偏航机动新条款——方向舵往复偏转,本文首先对两种偏航机动条款分别进行分析;然后考虑控制律进行偏航机动情况机动仿真计算;最后通过比较分析飞机响应运动参数及垂尾载荷计算结果,并分析控制律对偏航机动载荷的影响。结果表明:对于偏航机动,考虑控制律后飞机的响应幅度有所缓减,导致垂尾载荷有所降低;对于偏航机动新条款,由于方向舵反向偏转导致侧滑角贡献和方向舵偏度贡献垂尾载荷两者叠加,从而导致垂尾载荷大幅增加;P-Beta控制律有效降低了方向舵往复偏转的垂尾载荷。 展开更多
关键词 偏航机动 方向舵往复偏转 控制律 垂尾载荷 机动仿真
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Imaging simulation and analysis of attitude jitter effect on topographic mapping for lunar orbiter stereo optical cameras
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作者 CHEN Chen TONG Xiao-Hua +4 位作者 LIU Shi-Jie YE Zhen HUANG Chao-Wei WU Hao ZHANG Han 《红外与毫米波学报》 SCIE EI CAS CSCD 北大核心 2024年第5期722-730,共9页
The geometric accuracy of topographic mapping with high-resolution remote sensing images is inevita-bly affected by the orbiter attitude jitter.Therefore,it is necessary to conduct preliminary research on the stereo m... The geometric accuracy of topographic mapping with high-resolution remote sensing images is inevita-bly affected by the orbiter attitude jitter.Therefore,it is necessary to conduct preliminary research on the stereo mapping camera equipped on lunar orbiter before launching.In this work,an imaging simulation method consid-ering the attitude jitter is presented.The impact analysis of different attitude jitter on terrain undulation is conduct-ed by simulating jitter at three attitude angles,respectively.The proposed simulation method is based on the rigor-ous sensor model,using the lunar digital elevation model(DEM)and orthoimage as reference data.The orbit and attitude of the lunar stereo mapping camera are simulated while considering the attitude jitter.Two-dimensional simulated stereo images are generated according to the position and attitude of the orbiter in a given orbit.Experi-mental analyses were conducted by the DEM with the simulated stereo image.The simulation imaging results demonstrate that the proposed method can ensure imaging efficiency without losing the accuracy of topographic mapping.The effect of attitude jitter on the stereo mapping accuracy of the simulated images was analyzed through a DEM comparison. 展开更多
关键词 topographic mapping lunar orbiter stereo camera attitude jitter imaging simulation digital elevation model
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汽车转弯高维非线性动力学特性研究 被引量:4
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作者 王威 李瑰贤 宋玉玲 《哈尔滨工程大学学报》 EI CAS CSCD 北大核心 2009年第6期676-680,685,共6页
车辆的转弯动力学特性是衡量车辆机动性能好坏的一个重要标准.通过建立汽车高维非线性动力学仿真模型,分析了悬架参数与轮胎参数对系统非线性动力学特性的影响,深入研究了车辆在特定转向角输入条件下的转弯非线性动力学响应;对四轮在不... 车辆的转弯动力学特性是衡量车辆机动性能好坏的一个重要标准.通过建立汽车高维非线性动力学仿真模型,分析了悬架参数与轮胎参数对系统非线性动力学特性的影响,深入研究了车辆在特定转向角输入条件下的转弯非线性动力学响应;对四轮在不同扭矩作用下车辆的转弯机动性进行了对比分析;引入LuG re模型,充分考虑了轮胎的非线性特性,悬架单元采用绝对值型非线性弹性力与分段线性阻尼力,详细计算了车辆转弯时滚转角加速度、偏航角加速度、车体质心加速度、轮胎摩擦力的变化规律,应用M atlab6.5得到了具体的仿真结果;对确定车辆的横向动力学控制、转弯动力学性能预测及轮胎的磨损程度预测具有一定的指导意义. 展开更多
关键词 汽车动力学建模 转弯非线性动力学 非线性悬架参数 非线性LuGre模型 机动仿真
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Design and Simulation of Controller for Hyper Velocity Kinetic Energy Missile 被引量:2
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作者 康长赓 雷成 刘藻珍 《Journal of Beijing Institute of Technology》 EI CAS 2000年第1期107-112,共6页
The controller design and digital simulation for the hyper velocity kinetic energy missile is investigated. A mathematical model of the trajectory deviation from the line of sight was established, the guidance closed ... The controller design and digital simulation for the hyper velocity kinetic energy missile is investigated. A mathematical model of the trajectory deviation from the line of sight was established, the guidance closed loop was compensated with a phase advance lag corrective network, a selecting algorithm of the attitude control motors used to steer the missile's attitude was presented. In the presence of a wide variety of disturbances the results of digital simulation are satisfactory to circular error probability(CEP) being less than 0 5?m. The steering scheme utilizing attitude control motors as actuators to control the attitude of the missile is feasible. 展开更多
关键词 hyper velocity missile guidance missile control attitude control motor SIMULATION
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舰载螺旋桨运输机发动机短舱飞行载荷设计 被引量:2
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作者 马凯超 唐长红 +2 位作者 张建叶 牛孝飞 范庆志 《西北工业大学学报》 EI CAS CSCD 北大核心 2020年第6期1249-1256,共8页
舰载螺旋桨运输机布局紧凑,发动机短舱尺寸和质量较大,受螺旋桨滑流影响显著,飞行载荷问题突出,国内设计经验仍显不足。研究了某飞机发动机短舱的气动载荷、惯性载荷、陀螺力矩等设计方法及相关的设计规范约束与全机机动仿真技术。首先... 舰载螺旋桨运输机布局紧凑,发动机短舱尺寸和质量较大,受螺旋桨滑流影响显著,飞行载荷问题突出,国内设计经验仍显不足。研究了某飞机发动机短舱的气动载荷、惯性载荷、陀螺力矩等设计方法及相关的设计规范约束与全机机动仿真技术。首先通过对规范的理解和选择确定短舱飞行载荷设计范围;建立机动仿真模型,获得短舱典型载荷工况;通过CFD方法获得有、无滑流影响的短舱压力分布数据;计算、筛选短舱的设计载荷与设计载荷工况;对比有/无滑流影响的气动载荷计算结果。研究表明:短舱的设计载荷工况出现在最大法向载荷系数(n Z)下的急剧俯仰机动、设计俯冲速度(V D)下的偏航机动、最大着舰质量下的发动机最大拉力等情况中;短舱侧向以气动载荷为主;法向以惯性载荷为主,极值情况下惯性力超过气动力4倍;某些机动/状态下,螺旋桨滑流可使短舱总气动力增大90%以上,靠近螺旋桨区域增幅更大。 展开更多
关键词 舰载螺旋桨运输机 发动机短舱 气动载荷 惯性载荷 设计规范 机动仿真 螺旋桨滑流 设计载荷工况
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Synthetic Performance Simulation of E-Car HS2000
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作者 孙立清 孙逢春 张承宁 《Journal of Beijing Institute of Technology》 EI CAS 2000年第4期422-427,共6页
The simulation model of the E car HS2000 including the permanent magnetic direct current motor with the augment magnet winding is constructed based on tests in order to simulate the synthetic performance of the elec... The simulation model of the E car HS2000 including the permanent magnetic direct current motor with the augment magnet winding is constructed based on tests in order to simulate the synthetic performance of the electric car. The performance of E car HS2000 is analyzed by means of modeling and programming according to data acquired during tests. The simulation results show that the performance of E car HS2000 is successfully predicted and the model and the corresponding simulation software are feasible for simulating E cars. They can be used as effective tools for analyzing the performance parameters as well as specifications of E cars during prototype stage. 展开更多
关键词 E car simulation model of motor synthetic performance SIMULATION
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Simulation of Restraint System Performance upon the Occupant's Response During Impact
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作者 孙立清 林逸 孙逢春 《Journal of Beijing Institute of Technology》 EI CAS 1999年第2期96-102,共7页
Aim To study the influence of restraint system performance upon the occupant's response during impact, and provide a scientific base for occupant restraint system design. Methods \ In the light of basic th... Aim To study the influence of restraint system performance upon the occupant's response during impact, and provide a scientific base for occupant restraint system design. Methods \ In the light of basic theory of multibody system dynamics and impact dynamics on the basis of classical theory of impact, R W method is adopted to construct the vehicle occupant system model consisting of fourteen rigid bodies, thirty seven DOFs and slip joints for the simulation. A software named SVC3D(3 dimensional simulation of vehicle crash) is developed in the FORTRAN language. Results\ The results of simulation have a good coincidence with those of tests and the restraint system with low elongation webbing and equipped with pretensioner provides better restraint effect for the occupant. Conclusion\ The model of vehicle occupant multibody system and SVC3D are suitable for use. Occupant should be belted with low elongation webbing to a certain degree and occupant restraint system should be equipped with pretensioner. 展开更多
关键词 vehicle occupant multibody system model multibody system dynamics impact dynamics computer simulation vehicle passive safety
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ENHANCED UNSTEADY AND NONLINEAR ROTOR WAKE MODEL FOR REAL-TIME FLIG HT SIMULATION 被引量:2
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作者 孙传伟 高正 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI 2003年第1期12-16,共5页
WT5 'BZThis paper presents an unsteady and nonlinear wake model based on th e widely used Peters He finite state dynamic wake model with improvements. The swirl component in the tip trace plane (TTP) can be pr... WT5 'BZThis paper presents an unsteady and nonlinear wake model based on th e widely used Peters He finite state dynamic wake model with improvements. The swirl component in the tip trace plane (TTP) can be predicted, nonlinear items are added into the linear theory, and the old small angle assumption use d in matrix prediction is removed. All of these enha ncements are aimed at the low speed flight phase and formulations for the induce d velocity field just in the TTP frame are derived. The corresponding FORTRAN pr ogram is tested and optimized for the real time applications on PCs. 展开更多
关键词 HELICOPTER ROTOR WAKE dynamics inflow
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A New Simulation Method for 3D Propellant Grain Burn Analysis of Solid Rocket Motor
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作者 方蜀州 胡克娴 张平 《Journal of Beijing Institute of Technology》 EI CAS 1995年第2期214+207-214,共9页
Describes a new computer program (Regress-3D) to simulate the regression of complex 3D grain cavity and calculate the burning surface area. It has a large region of applicability in solid rocket motor design and has... Describes a new computer program (Regress-3D) to simulate the regression of complex 3D grain cavity and calculate the burning surface area. It has a large region of applicability in solid rocket motor design and has made new improvements compared with other available codes. User can easily and rapidly build his initial grain shapes and then obtain geometric information of his design. Considering with the calclulting results, redesigning can be performed as desire until reaching at the satisfied result. Advantages and disadvantages of this method are also discussed. 展开更多
关键词 solid propellant rocket engines propellant grains computerized simulation COMBUSTION
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Simulation of Dynamic Electromagnetic Interference Environment for Unmanned Aerial Vehicle Data Link 被引量:10
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作者 郭淑霞 董中要 +1 位作者 胡占涛 胡楚峰 《China Communications》 SCIE CSCD 2013年第7期19-28,共10页
In order to test the anti-interference ability of an Unmanned Aerial Vehicle(UAV) data link in a complex electromagnetic environment,a method for simulating the dynamic electromagnetic interference of an indoor wirele... In order to test the anti-interference ability of an Unmanned Aerial Vehicle(UAV) data link in a complex electromagnetic environment,a method for simulating the dynamic electromagnetic interference of an indoor wireless environment is proposed.This method can estimate the relational degree between the actual face of an UAV data link in an interface environment and the simulation scenarios in an anechoic chamber by using the Grey Relational Analysis(GRA) theory.The dynamic drive of the microwave instrument produces a real-time corresponding interference signal and realises scene mapping.The experimental results show that the maximal correlation between the interference signal in the real scene and the angular domain of the radiation antenna in the anechoic chamber is 0.959 3.Further,the relational degree of the Signal-toInterference Ratio(SIR) of the UAV at its reception terminal indoors and in the anechoic chamber is 0.996 8,and the time of instrument drive is only approximately 10 μs.All of the above illustrates that this method can achieve a simulation close to a real field dynamic electromagnetic interference signal of an indoor UAV data link. 展开更多
关键词 UAV data link dynamic electromagnetic interference GRA relational degree scene mapping instrument driver
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Computer simulation of active suspension based on the full-vehicle model 被引量:2
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作者 李军 CHEN Shanguo 《Journal of Chongqing University》 CAS 2002年第2期24-27,共4页
Abstract: The current method to solve the problem of active suspension control for a vehicle is often dealt with a quarter-car or half-car model. But it is not enough to use this kind of model for practical applicatio... Abstract: The current method to solve the problem of active suspension control for a vehicle is often dealt with a quarter-car or half-car model. But it is not enough to use this kind of model for practical applications. In this paper, based on considering the influence of factors such as, seat and passengers, a MDOF(multi-degree-of-freedom) model describing the vehicle motion is set up. The MODF model, which is 8DOF of four independent suspensions and four wheel tracks, is more applicable by comparison of its analysis result with some conventional vehicle models. Therefore, it is more suitable to use the 8DOF full-car model than a conventional 4DOF half-car model in the active control design for car vibration. Based on the derived 8DOF model, a controller is designed by using LQ (linear quadratic ) control theory, and the appropriate control scheme is selected by testing various performance indexes. Computer simulation is carried out for a passenger car running on a road with step disturbance and random road disturbance expressed by Power Spectral Density (PSD). Vibrations corresponding to ride comfort are derived under the foregoing road disturbances. The response results for uncontrolled and controlled system are compared. The response of vehicle vibration is greatly suppressed and quickly damped, which testifies the effect of the active suspension. The results achieved for various controllers are compared to investigate the influence of different control schemes on the control effect. 展开更多
关键词 active suspension LQ control 8DOF model
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A tunable fuzzy logic controller for the vehicle semi-active suspension system
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作者 方子帆 DENG +1 位作者 Zhaoxiang 《Journal of Chongqing University》 CAS 2002年第2期16-19,共4页
On the basis of analyzing the system constitution of vehicle semi-active suspension, a 4-DOF (degree of freedom) dynamic model is established. A tunable fuzzy logic controller is designed by using without quantificati... On the basis of analyzing the system constitution of vehicle semi-active suspension, a 4-DOF (degree of freedom) dynamic model is established. A tunable fuzzy logic controller is designed by using without quantification method and taking into account the uncertainty, nonlinearity and complexity of parameters for a vehicle suspension system. Simulation to test the performance of this controller is performed under random excitations and definite disturbances of a C grade road, and the effects of time delay and changes of system parameters on the vehicle suspension system are researched. The numerical simulation shows that the performance of the designed tunable fuzzy logic controller is effective, stable and reliable. 展开更多
关键词 VEHICLE semi-active suspension system fuzzy logic control SIMULATION
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