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小型无人机飞行姿态测量系统的设计 被引量:5
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作者 赵海生 胥效文 《计算机测量与控制》 CSCD 北大核心 2012年第3期583-585,共3页
飞行姿态是无人机飞行时最重要的参数之一,针对现有多数姿态测量系统体积大、功耗高、续航时间短,并不适合应用于小型或微型无人机上等问题,提出了一种基于DSP的小型化无人机飞行姿态测量的设计方案;完成了微固态陀螺实时数据采集,并通... 飞行姿态是无人机飞行时最重要的参数之一,针对现有多数姿态测量系统体积大、功耗高、续航时间短,并不适合应用于小型或微型无人机上等问题,提出了一种基于DSP的小型化无人机飞行姿态测量的设计方案;完成了微固态陀螺实时数据采集,并通过四阶Runge-Kutta方法对其姿态角进行了求解;给出了姿态测量系统各模块的设计思想及基于μC/OS-Ⅱ的软件设计流程;与NAV440CA-200型IMU对比结果显示,在35秒的测试时间内滚转角相对误差为0.5°,俯仰角相对误差为0.4°;试验结果表明,该姿态测量系统具有较高的测量精度、体积小、功耗低等特点,满足设计需要。 展开更多
关键词 飞行姿态 UC/OS-Ⅱ 微固态陀螺 runge--kutta
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Friction phenomena in a two-dimensional Frenkel-Kontorova model 被引量:1
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作者 林麦麦 段文山 陈建敏 《Chinese Physics B》 SCIE EI CAS CSCD 2010年第2期361-366,共6页
By using the molecular dynamic simulation method with a fourth-order Runge--Kutta algorithm, a two-dimensional dc- and ac-driven Frenkel--Kontorova (FK) model with a square symmetry substrate potential for a square ... By using the molecular dynamic simulation method with a fourth-order Runge--Kutta algorithm, a two-dimensional dc- and ac-driven Frenkel--Kontorova (FK) model with a square symmetry substrate potential for a square lattice layer has been investigated in this paper. For this system, the effects of many different parameters on the average velocity and the static friction force have been studied. It is found that not only the amplitude and frequency of ac-driven force, but also the direction of the external driving force and the misfit angle between two layers have some strong influences on the static friction force. It can be concluded that the superlubricity phenomenon appears easily with a larger ac amplitude and lower ac frequency for some special direction of the external force and misfit angle. 展开更多
关键词 Frenkel--Kontorova model static friction force runge--kutta method
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