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2007081312413982768
- 基于载波相位三差的航天器GPS/INS组合姿态算法-Based on carrier phase III spacecraft poor GPS/INS Attitude Algorithm portfolio
conicalmotion
- 采用四元数法的标准圆锥运动的姿态角仿真程序，。-Quaternion method using the standard cone movement attitude angle simulation procedures.
ballastic_missile_free_flying_simulation
- 利用OpenGL三维图形实时交互技术,在VC++中编程,实现了不同输入条件下的导弹自由段飞行弹道与飞行姿态仿真,包括导弹建模、以及由云彩绘制和流动效果组成的云彩的建模。-Use OpenGL real-time interactive three-dimensional graphics technology, VC++ In programming, to achieve a different input under the conditions of the free flights of
AttDet_23_Oct_2008
- 利用gps多天线载波相位技术，确定姿态软件。-The use of multi-antenna gps carrier phase technology, attitude determination software.
integration_of_attitudes
- 利用三轴角速率型号和三轴加速度计信号结合扩展卡尔曼滤波实现三个姿态角度的融合-The use of three-axis angular velocity model and three-axis accelerometer signal extended Kalman filter combined with the realization of the integration of the three attitude angles
3DMeasuringObjectPose
- 用惯量椭圆法实现轴对称目标的三维姿态测量新方法-Application of Ellipse of Inertia in Measuring the Object′s 3D Pose from Mono-View
ear3
- 国际会议上的关于人耳图像识别的论文： 改进的局部线性嵌入多姿态耳识别方法-MULTI-POSE EAR RECOGNITION BASED ON IMPROVED LOCALLY LINEAR EMBEDDING
mimu
- 自己仿真的四元数法的龙格库塔的姿态解算matlab仿真-Their simulation method quaternion attitude Runge-Kutta solver matlab simulation
hrrf2scatterIn2D
- 基于多姿态一维距离像(HRRP)的二维散射中心重构matlab仿真算法-Reconstruction of 2D scattering center
Navigation
- 利用比力、加速度信息解算出惯性导航所需的速度、位置和姿态信息-Than the use of force, acceleration of information required for inertial navigation solution to calculate the speed, position and attitude information
796e50c2-1775-4730-8213-2225004ca5c1
- 利用matlab数值计算的强大功能和,建模容易实现的特点"进行了捷联式惯性导航系统的仿真研究,对四元数及姿态矩阵等的解算采用编程实现"陀螺仪和加速计的建模用.-Matlab numerical calculation using the power and, modeling the characteristics of easy to implement " a strapdown inertial navigation system of the simulation study a
dubsi10-2
- 飞机仿真软件包dubsi10-2，可以与FDC tool（本站已有）一起使用的matlab/simulink仿真软件，主要对飞机的滚转姿态控制进行仿真研究，内有丰富的案例。-The Dutchroll Blockset for Simulink, DUBSI, is a stand-alone version of the blocklibrary BLOCKLIB_MISC in version 2.0 (or later) of the Flight Dynamics and Con
OMNeTbasedsatelliteposecontrolsimulation
- 针对三轴稳定卫星的姿态控制系统,在离散事件仿真平台OMNeT ++的 基础上,建立了一个以星敏感器和陀螺为敏感器,反作用飞轮为执行机构的闭环 控制仿真系统。采用双矢量定姿算法和P ID控制算法,对该卫星在对地定向模 式下的控制精度进行了仿真。仿真结果清晰地反映了星敏感器和反作用飞轮输 出延时对控制精度的影响。整个仿真系统符合面向对象和模块化的程序设计理 念,并实现了仿真程序的重用。-For the three-axis stabilized satellite attitu
jingtai
- 捷联惯惯性导航的C程序实现，四元数表示姿态，静态下进行试验，MATLAB进行图像处理，包含原始数据。-Strapdown inertial navigation of the C programs used to achieve, said the attitude quaternion, static tests under, MATLAB for image processing, including raw data.
xiaotuoluo
- 捷联惯导的C程序实现，四元数进行姿态更新，MATLAB进行图像处理，包含原始数据。-SINS of the C program implementation, quaternion for attitude update, MATLAB for image processing, including raw data.
PID
- 航天器姿态控制PID控制仿真程序，加入干扰值。-PID control of spacecraft attitude control simulation program, by adding the value of interference.
Face_test_luminance
- 结合人脸肤色和发色进行的人脸检测，可以忽略人脸的姿态表情，不用进行人脸特征的定位-Combination of face color and hair color for face detection, facial gesture can ignore the expression, do not carry out the positioning of facial features
201003tecplot
- 简介卫星姿态控制系统的模型，并针对该模型分析故障发生的特点，故 障诊断的难点，以及可能发生故障的部位和故障的类型，给出故障检测的方法。-Introduction of satellite attitude control system model and the model for the analysis of the characteristics of faults, fault diagnosis of the difficulties, and possible failure l
planecontrol
- 飞机姿态的系统调整，依据机头倾角，进行反馈控制-simulink