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升力式再入飞行器无控飞行溅落区仿真研究
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作者 赵璟 《军民两用技术与产品》 2016年第4期28-28,共1页
飞行器在无控飞行状态下可能的着陆区域称为溅落区。针对升力式再入飞行器在典型受损机体形态下的溅落区问题,本文采用面元法对不同机体形态进行了气动建模,基于气象观测数据建立了大气扰动模型,针对飞行器典型工况点建立飞行状态散... 飞行器在无控飞行状态下可能的着陆区域称为溅落区。针对升力式再入飞行器在典型受损机体形态下的溅落区问题,本文采用面元法对不同机体形态进行了气动建模,基于气象观测数据建立了大气扰动模型,针对飞行器典型工况点建立飞行状态散布模型,建立了六自由度运动模型对升力式再入飞行器进行蒙特卡洛仿真。根据仿真结果,分析了大气扰动、气动模型偏差、初始状态散布等因素对无控升力式再入飞行器溅落区的影响。 展开更多
关键词 升力式再入飞行 溅落区 无控飞行 六自由度 数学仿真
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基于改进混杂扩展卡尔曼滤波的炮弹阻力系数辨识 被引量:4
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作者 杨靖 常思江 王中原 《弹道学报》 CSCD 北大核心 2017年第1期28-33,共6页
针对利用炮弹飞行数据辨识阻力系数的问题,提出了一种改进形式的混杂扩展卡尔曼滤波(IHEKF)方法。引入虚拟过程噪声并且在每个时间步长对称化协方差矩阵,避免了混杂扩展卡尔曼滤波在实际应用中由于系统建模误差及弹载计算机的精度有限... 针对利用炮弹飞行数据辨识阻力系数的问题,提出了一种改进形式的混杂扩展卡尔曼滤波(IHEKF)方法。引入虚拟过程噪声并且在每个时间步长对称化协方差矩阵,避免了混杂扩展卡尔曼滤波在实际应用中由于系统建模误差及弹载计算机的精度有限引起的发散问题,提高了阻力系数辨识的鲁棒性。数值仿真结果表明:当建模误差可以忽略不计时,采用IHEKF能以高精度辨识出阻力系数;当建模误差较大时,采用IHEKF具有较好的鲁棒性。 展开更多
关键词 炮弹 无控飞行 参数辨识 扩展卡尔曼滤波
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GUIDANCE AND CONTROL FOR AUTOMATIC LANDING OF UAV 被引量:1
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作者 曹云峰 陶勇 沈勇璋 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI 2001年第2期229-235,共7页
A scheme of guidance and control is presented to meet the requirements for automatic landing of unmanned aerial vehicles (UAVs) based on the airborne digital flight control system and radio tracker on ground station. ... A scheme of guidance and control is presented to meet the requirements for automatic landing of unmanned aerial vehicles (UAVs) based on the airborne digital flight control system and radio tracker on ground station. An automatic landing system is realized for an unmanned aerial vehicle. The results of real time simulation and flight test are given to illustrate the effectiveness and availability of the scheme. Results meet all the requirements for automatic landing of the unmanned aerial vehicle. 展开更多
关键词 automatic landing unmanned aerial vehicle GUIDANCE NAVIGATION flight control
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An optimization model of UAV route planning for road segment surveillance 被引量:1
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作者 刘晓锋 关志伟 +1 位作者 宋裕庆 陈大山 《Journal of Central South University》 SCIE EI CAS 2014年第6期2501-2510,共10页
Unmanned aerial vehicle(UAV)was introduced to take road segment traffic surveillance.Considering the limited UAV maximum flight distance,UAV route planning problem was studied.First,a multi-objective optimization mode... Unmanned aerial vehicle(UAV)was introduced to take road segment traffic surveillance.Considering the limited UAV maximum flight distance,UAV route planning problem was studied.First,a multi-objective optimization model of planning UAV route for road segment surveillance was proposed,which aimed to minimize UAV cruise distance and minimize the number of UAVs used.Then,an evolutionary algorithm based on Pareto optimality technique was proposed to solve multi-objective UAV route planning problem.At last,a UAV flight experiment was conducted to test UAV route planning effect,and a case with three scenarios was studied to analyze the impact of different road segment lengths on UAV route planning.The case results show that the optimized cruise distance and the number of UAVs used decrease by an average of 38.43% and 33.33%,respectively.Additionally,shortening or extending the length of road segments has different impacts on UAV route planning. 展开更多
关键词 unmanned aerial vehicle traffic surveillance route planning multi-objective optimization evolutionary algorithm
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Research on the Unmanned Aerial Vehicle Adaptive Control System based on Fuzzy Control and Chaos Mechanics
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作者 Jianqiong Xu 《International Journal of Technology Management》 2016年第8期52-54,共3页
In this paper, we conduct research on the unmanned aerial vehicle adaptive control system based on fuzzy control and chaosmechanics. Four rotor aircraft is a kind of nonlinear systems with underactuated, strong coupli... In this paper, we conduct research on the unmanned aerial vehicle adaptive control system based on fuzzy control and chaosmechanics. Four rotor aircraft is a kind of nonlinear systems with underactuated, strong coupling characteristic. Although in existing research,through the design of the control algorithm effectively inhibits both for fl ight control effect, but not fundamentally eliminate the effect of aircraft.Dynamic model of unmanned helicopter fl ight control system design is very approximate, need to gradually improve the modeling accuracy, soas to get the exact autonomous fl ight control, so you need to practice constantly required to modeling in the fl ight information, so the unmannedhelicopter fl ight control system to have the ability to retrieve information modeling. This paper proposes the new idea on the issues that will bemeaningful. 展开更多
关键词 Unmanned Aerial Vehicle Adaptive Control SYSTEM Fuzzy Control Chaos Mechanics.
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Trophallaxis network control approach to formation flight of multiple unmanned aerial vehicles 被引量:17
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作者 DUAN HaiBin LUO QiNan YU YaXiang 《Science China(Technological Sciences)》 SCIE EI CAS 2013年第5期1066-1074,共9页
A novel network control method based on trophaUaxis mechanism is applied to the formation flight problem for multiple un- manned aerial vehicles (UAVs). Firstly, the multiple UAVs formation flight system based on tr... A novel network control method based on trophaUaxis mechanism is applied to the formation flight problem for multiple un- manned aerial vehicles (UAVs). Firstly, the multiple UAVs formation flight system based on trophallaxis network control is given. Then, the model of leader-follower formation flight with a virtual leader based on trophallaxis network control is pre- sented, and the influence of time delays on the network performance is analyzed. A particle swarm optimization (PSO)-based formation controller is proposed for solving the leader-follower formation flight system. The proposed method is applied to five UAVs for achieving a 'V' formation, and a series of experimental results show its feasibility and validity. The proposed control algorithm is also a promising control strategy for formation flight of multiple unmanned underwater vehicles (UUVs), unmanned ground vehicles (UGVs), missiles and satellites. 展开更多
关键词 unmanned aerial vehicle (UAV) trophaHaxis network control formation flight particle swarm optimization (PSO)
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Determining the oil weighting factor of oil-water emulsion based on the fractional Weierstrass scattering model
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作者 LI Yang TAO Ran SHENG XinQing 《Science China Earth Sciences》 SCIE EI CAS 2014年第8期1780-1789,共10页
The formation of oil-water emulsion often occurs when oil is spilled into the ocean. Oil weighting factor of oil-water emulsion is one of the most important parameters for emergent oil-spill microwave monitoring. A ne... The formation of oil-water emulsion often occurs when oil is spilled into the ocean. Oil weighting factor of oil-water emulsion is one of the most important parameters for emergent oil-spill microwave monitoring. A new method is proposed here to evaluate the oil weighting factor based on fractional Weierstrass scattering model. By using the proposed method, we analyze the Uninhabited Aerial Vehicle Synthetic Aperture Radar(UAVSAR) L-band fully polarimetric data acquired during 2010 Deepwater Horizon oil spill disaster event in the Gulf of Mexico. The result shows that our method performs well in evaluating oil weighting factor of oil-covered area. 展开更多
关键词 oil spill Uninhabited Aerial Vehicle Synthetic Aperture Radar (UAVSAR) Deepwater Horizon (DWH) fractionalWeierstrass scattering model
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