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Description: GPS导航系统的matlab程序（精度很高哦） -GPS navigation systems matlab program (oh, high precision)
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Size: 1024 |
Author: tianxingjian |
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Description: Development of GPS INS Loop for UAV
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Size: 2971648 |
Author: ztlits |
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Description: This project will use the Arduino Diecimila as the hardware platform to control a quadrocopter. Software coding will be done in the Arduino environment. The primary goal for this quadrocopter will be to create a low cost flying vehicle which integrates gyros, accelerometers and a GPS for attitude control compatible with a 2.4GHz RC controller like the Spektrum DX7. A secondary goal would be to make this an autonomous UAV, which can fly to programmed waypoints without pilot intervention.
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Size: 53248 |
Author: marshallab |
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Description: 关于GPS/INS组合导航的matlab仿真程序 大家共同学习下-On GPS/INS Integrated Navigation System of the matlab simulation program to study under the common
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Size: 634880 |
Author: zhoufeng |
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Description: 基于GPS仿真器的无人机导航系统半物理仿真-GPS-based navigation system for UAV simulator loop simulation
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Size: 273408 |
Author: zin567 |
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Description: 无人机自驾仪设计本文介绍了自驾仪的结构及GPS接收机- UAV autopilot design the passage mainly about the struction of atuopilot
and GPS receiver
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Size: 47104 |
Author: 南天 |
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Description: The open source project DSP_INS is an inertial navigation system on the TI DSP
platform TMS320F28335 with MEMS inertial sensors and commercial GPS module. Inertial
sensors are actually used only for estimating attitude, heading and velocity.
Position information totally comes from GPS (see Q2 in FAQ part). Currently the
MEMS IMU (Inertial Measurement Unit) ADIS16355 and GPS module u-blox LEA-5H
are supported. DSP_INS also reads magnetic field data from HONEYWELL HMC1051/1052.
You can also use the latest IMU module ADIS16405, which also contains magnetic field
sensors.
There is a 10-order extended Kalman filter in DSP_INS, which takes angular velocity,
acceleration, magnetic field, and GPS velocity as inputs. It provides outputs
including angular velocity, acceleration, attitude, heading, velocity, and position
(from GPS) every 10 milliseconds. DSP_INS is proved to be effective and reliable in
several robot and UAV projects.
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Size: 1682432 |
Author: snthej |
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Description: 国外网站www.openpilot.com开源的一款无人机GPS辅助INS导航算法程序，据说目前很多国内无人机都是使用的这套导航算法，对研究惯导的朋友可能会有帮助-Foreign site www.openpilot.com open source is a UAV GPS Aided INS navigation algorithm program, said many domestic UAV use this navigation algorithm, to study INS friends may be helpful
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Size: 45056 |
Author: 刘小码 |
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Description: Altitude location for UAV by using federated filter
is discussed, the fourth structure is selected, because its two
sub-filters involving altitude sensor and the difference Global
Positioning System (d-GPS) respectively are fully isolated from
each other and thus make the federated filter more fault-tolerant
and better in real-time performance. Data fusion based on this
federated filter was simulated. When the d-GPS is working
normally and simulation results show that values estimated by
data fusion base on federated filter are very close to real values
and the variance of federated filter converges to 10m. When the
electromagnetic environment is very bad, as is usually the case in
war zone, the d-GPS is silent for a long time, variance based on
federated filter converges to 13m, bigger than the 10m.
Compared with previous paper variance based on Kalman
converges to 15m, higher than the 13m. Federated filter can give
much more accurate estimation than Kalman filter.
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Size: 328704 |
Author: Clovis |
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Description: GPS navigation system for UAVs-GPS navigation system for UAV
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Size: 346112 |
Author: hzt |
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Description: 无人机地面遥测接收站源码，基于AT89C2051，接收无人机下行的状态数据，同时解析GPS数据，送给主控显示-UAV ground station telemetry source, based on AT89C2051, UAV downlink receiving status data, and GPS data analysis, and gave master display
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Size: 26624 |
Author: zzl |
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Description: INS\GPS navigation for UAV
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Size: 2972672 |
Author: toufik1629 |
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Description: 本压缩文件包是APM开源飞控代码，包括APMrover2,ArduCopter,ArduPlane，即地面车辆，多旋翼无人机，直升机的开源飞控程序，包含大量库文件，实现不同机型飞行器的飞行控制，可以设置不同飞行模式，利用GPS导航进行正确定位，实现对飞行器的多种控制。-The compressed file packet is APM open source control code, including APMrover2, ArduCopter, ArduPlane, namely ground vehicle, multi rotor UAV helicopter flight control program, open source, contains a large number of library files, realization of flight control of different types of aircraft, can set different flight mode, carry on the correct localization using GPS navigation, to achieve a variety of aircraft control.
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Size: 6779904 |
Author: jenny |
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Description: 拆解配备GPS的小型遥控飞机（派诺特的无人机）-Small remote cannibalized aircraft equipped with GPS (parrot UAV)
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Size: 224256 |
Author: 黄建 |
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Description: JD-GCS01无人机地面站系统
产品介绍
JD-GCS01无人机地面站系统是无人机自动驾驶仪配套地面站指挥控制系统，内置60KM远距离通讯数传电台、图传及图像采集卡、GPS/BD双频卫星接收机、摇杆，具有便携、集成化高、处理能力强等特点。
电源：内置锂离子聚合物电池，可实现220V/电池双供电模式。
充电功耗：<15W；电池连续工作时间：>2h
外形尺寸：510x420x200mm 重量：6kg-JD-GCS01 UAV Ground Station System
Product introduction
JD-GCS01 no UAV Ground Station system is UAV automatic driving instrument supporting the ground station command and control system, built-in 60km long distance data communication transmission radio, image transmission and image acquisition card, GPS/BD dual frequency satellite receiver, a rocker, with portable, high integration, strong capability of processing characteristics.
Power supply: built in lithium ion polymer battery, 220V/ battery can realize the dual power supply mode.
Charging power consumption: <15W continuous working time of the battery: >2h
Size: 510x420x200mm weight: 6kg
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Size: 171008 |
Author: 黄磊 |
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Description: GPS在无人机上的具体工作过程的程序，可以对位人机的位置实时监测-GPS in unmanned aerial vehicle (uav) on the specific working process of the program, can para man-machine real-time monitoring
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Size: 6144 |
Author: 邓丽敏 |
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Description: 北斗GPS双模在利用“当前”统计模型并利用kalman滤波时，其系统噪声和观测噪声未知且时变，而且加速度上下限不能自适应于未知运动规律的无人飞行器当前加速度，导致导航精度降低。该程序是相应的MATLAB仿真程序。(Beidou GPS dual mode uses the "current" statistical model and the Kalman filter. Its system noise and observation noise are unknown and time-varying, and the upper and lower limits of acceleration can not be adapted to the current acceleration of the unknown motion law of the UAV, resulting in the reduction of navigation accuracy. The program is the corresponding MATLAB simulation program.)
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Size: 9216 |
Author: Wayne0830 |
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