首页> 外文会议>International Conference for Internet Technology and Secured Transactions >A design of sounding rocket video processing system based on wavelet transform compression algorithm
【24h】

A design of sounding rocket video processing system based on wavelet transform compression algorithm

机译:基于小波变换压缩算法的探空火箭视频处理系统设计

获取原文

摘要

In order to construct an integrated sounding rocket experimental platform and to record the status of the sounding rocket as well as onboard payloads, an onboard video processing system based on the wavelet transform compression algorithm is designed in this paper. Specifically, the system utilizes a compression algorithm based on the bi-orthogonal (9, 7) discrete wavelet transform and implements field independent subband coding. Moreover, the system supports 10∶1 to 200∶1 real-time compression, and the frame rate is at range of 1fps to 25 fps (frame-per-second). To achieve a near constant compressed bit rate, the system adopts the Proportional-Integral-Derivative (PID) algorithm to conduct quantization control. The embedded system architecture, based on ARM and FPGA, is used to design the hardware circuit, which is characterized with the features of simple structure, high integration level and strong flexibility. Practical tests indicate that the proposed system has the characteristics of low power dissipation, low cost, small size, high reliability, high and low temperature resistance, vibration and impact resistance, which can withstand hostile environment on sounding rocket and it is very suitable for sounding rocket application.
机译:为了构建一个集成的探空火箭实验平台并记录其状态以及机载有效载荷,设计了一种基于小波变换压缩算法的机载视频处理系统。具体地,该系统利用基于双正交(9、7)离散小波变换的压缩算法,并实现与场无关的子带编码。此外,系统支持10:1到200:1的实时压缩,并且帧速率在1fps到25fps(每秒帧)的范围内。为了实现接近恒定的压缩比特率,系统采用比例积分微分(PID)算法进行量化控制。采用基于ARM和FPGA的嵌入式系统架构设计硬件电路,具有结构简单,集成度高,灵活性强的特点。实际测试表明,该系统具有功耗低,成本低,体积小,可靠性高,耐高低温,抗振动,抗冲击的特点,可以承受测深火箭的恶劣环境,非常适合测深火箭应用。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号