减少相邻位平面间冗余度的加密图像可逆信息隐藏

目的针对现有的加密域可逆信息隐藏算法在对位平面压缩时未能充分利用位平面间的相关性的问题,为了降低位平面的压缩率从而提高嵌入容量,提出一种减少相邻位平面间冗余度的加密域可逆信息隐藏算法。方法算法将图像进行分块并将块的位置进行置乱,置乱并未改变位平面的块内像素的相关性,使得位平面的块同样利于压缩。将块置乱后的图像的高位平面与次高位进行异或操作后得到新的次高位平面,再用新的次高位异或比它低一位的位平面。依次对其余的低位平面进行同样的操作后得到新的低7个位平面,将它们与原始最高位相结合得到新的图像的8个位平面。使用BBE(binary-block embeding)算法对新的图像的位平面进行压缩为嵌入信息腾出空间。为了保证加密图像的安全性,对腾出空间后的图像进行异或加密。结果对相邻位平面进行异或后使除了最高位平面外的低位平面更平滑,减少了不能使用BBE算法压缩的块及压缩的不好的块的个数,更有利于用BBE算法对图像进行压缩。提出的算法与现有的基于位平面压缩的算法相比得到了较高的嵌入率,对不同纹理的图像而言,嵌入的容量平均提高了0. 4 bit/像素。结论实验结果表明,提出的算法在保证安全性的同时可以腾出更多的空间来嵌入额外的信息,在实际生活中能根据需求灵活地嵌入信息。嵌入的信息能无损地提取,且图像能完全恢复。总的来说,提出的算法具有良好的性能。

多频无线网络通信隐私信息实时隐藏方法仿真

针对当前隐私信息隐藏方法无法满足隐私信息隐藏实时性、高隐蔽性且嵌入容量大等通信需求,提出基于位平面压缩的多频无线网络通信隐私信息实时隐藏方法。以位压缩编码形式将隐私信息低位平面信息保留在压缩后的高位平面中。运用比特替换形式在低位平面嵌入密文,在嵌入域内按位重组隐私信息。接收端在密文域中采用模乘法逆元提取出密文,对其直接解密无损恢复出原始隐私信息。实验结果表明,所提方法能够有效避免隐私信息彼此覆盖,实现隐私信息的实时传输,且具有较高的嵌入容量。

基于Peano曲线扫描的大容量密文域可逆信息隐藏方案

针对现有密文域可逆信息隐藏算法中存在嵌入率低、安全性不足等问题进行了研究,提出了一种利用图像像素间相关性的大容量密文域可逆信息隐藏方案。首先利用图像位平面间相关性减小冗余,再使用Peano曲线对位平面进行扫描,利用游程霍夫曼编码对每个位平面进行压缩,而后利用图像高位信息对低位空间进行填充,最后用填充消息作为隐藏密钥对秘密信息异或加密实现嵌入。实验结果表明,该方法可完全可逆地恢复原始图像,平均最大嵌入容量达2.53 bpp。

Numerical Simulation of Coal Floor Fault Activation Influenced by Mining

By means of the numerical simulation software ANSYS, the activation regularity of coal floor faults caused by mining is simulated. The results indicate that the variation in horizontal, vertical and shear stresses, as well as the horizontal and vertical displacements in the upper and the lower fault blocks at the workface are almost identical. Influ- enced by mining of the floor rock, there are stress releasing and stress rising areas at the upper part and at the footwall of the fault. The distribution of stress is influenced by the fault so that the stress isolines are staggered by the fault face and the stress is focused on the rock seam around the two ends of the fault. But the influence in fault activation on the upper or the lower fault blocks of the workface is markedly different. When the workface is on the footwall of the fault, there is a horizontal tension stress area on the upper part of the fault; when the workface is on the upper part of the fault, it has a horizontal compressive stress area on the lower fault block. When the workface is at the lower fault block, the maximum vertical displacement is 5 times larger then when the workface is on the upper fault block, which greatly in- creases the chance of a fatal inrush of water from the coal floor.

Application of an Analytical Method to Locate a Mixing Plane in a Supersonic Compressor

In order to achieve greater pressure ratios, compressor designers have the opportunity to use transonic configurations. In the supersonic part of the incoming flow, shock waves appear in the front part of the blades and propagate in the upstream direction. In case of multiple blade rows, steady simulations have to impose an azimuthal averaging （mixing plane） which prevents these shock waves to extend upstream. In the present paper, several mixing plane locations are numerically tested and compared in a supersonic configuration. An analytical method is used to describe the shock pattern. It enables to take a critical look at the CFD （computational fluid dynamics） steady results. Based on this method, the shock losses are also evaluated. The good agreement between analytical and numerical values shows that this method can be useful to wisely forecast the mixing plane location and to evaluate the shift in performances due to the presence of the mixing plane.