![Scientific and technical journal «Priborostroenie»](/images/mag-pr.png)
HIGH-PERFORMANCE ALGORITHM FOR SIMULATION OF THE EARTH REMOTE SENSING RADAR SYSTEM ON A GRAPHICS PROCESSOR WITH PARALLEL ARCHITECTURE
![Scientific and technical journal «Priborostroenie»](/images/mag-pr.png)
Annotation
Methods of calculation acceleration in modeling radar systems with synthetic aperture on the GPU parallel architecture are considered. The simulation is based on a point model of the underlying surface. The modeling algorithm assumes preliminary calculation of the reflected signals with the increased sampling rate and subsequent approximation of obtained results to derive a hologram of the district model. It is shown that the time limit for hologram synthesis is defined as the product of number of processes in the block and the number of blocks in the lattice. The combination of these parameters is to be selected based on the architecture of the graphics accelerator. Results of simulations carried out on NVIDIA Tesla K20 GPU using CUDA are presented. Efficiency of the graphic accelerator application for modeling the RLS RSA is confirmed. Thus, in the case of a hologram for a 100x100 points model, the time gain is more than twenty times compared to calculations performed with a general-purpose processor.
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Articles in current issue
- FUNCTIONAL STABILITY OF NAVIGATION INFORMATION SYSTEMS
- MATHEMATICAL MODELS OF RELIABILITY OF NON-HERMETIC SPACE APPLIANCES OF RADIO-ELECTRONIC EQUIPMENT
- ASSESSMENT OF GEOMETRIC ACCURACY OF SATELLITE IMAGES OBTAINED BY THE EARTH REMOTE SENSING SYSTEMS IN VARIOUS RANGES OF THE ELECTROMAGNETIC SPECTRUM
- BASIC CONCEPTS OF A METHOD FOR COMPARATIVE EVALUATION OF TECHNICAL LEVEL OF UNIFIED SPACE PLATFORMS
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- METHODS, ALGORITHMS, AND TECHNOLOGIES FOR RECONFIGURATION OF ON-BOARD EQUIPMENT OF SMALL-SIZED SPACECRAFTS
- PROPOSALS FOR CREATION OF SATELLITE INVERSE RADIO TOMOGRAPHY SYSTEM
- TECHNOLOGY OF RELIABILITY ASSESSMENT FOR ELECTRONICS ELEMENTS, LONG FUNCTIONING UNDER CONDITIONS OF OUTER SPACE
- DEVELOPMENT OF SPACE PLASMA FLOW SENSOR WITH FOUR-SECTION COLLECTOR
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