Fiber-optic gyroscope strapdown inertial navigation computer based on DSP (Digital Signal Processor) and navigation calculating method thereof
A strapdown inertial navigation and fiber optic gyro technology, applied in the field of inertial navigation computers, can solve the problems of low navigation calculation efficiency and complex structure, and achieve the effects of low power consumption, strong computing power, and fast acquisition speed
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specific Embodiment approach 1
[0025] Specific implementation mode one: combine figure 1 Describe this embodiment, the fiber optic gyroscope strapdown inertial navigation computer based on DSP described in this embodiment,
[0026] It includes FPGA data acquisition module 1, DSP module 2, storage module 3 and communication module 4;
[0027] The DSP module 2 is connected with the FPGA data acquisition module 1 through the EMIFB interface, the storage signal input and output terminals of the storage module 3 are connected with the storage signal input and output terminals of the DSP module 2, and the communication signal input and output terminals of the communication module 4 communicate with the DSP module 2 Signal input and output connections;
[0028] The DSP module 2 is realized by using the chip TMS320C6713.
[0029] The FPGA data acquisition module is mainly composed of FPGA and its configuration circuit, and completes the acquisition of three-way gyroscope and three-way accelerometer navigation dat...
specific Embodiment approach 2
[0037] Specific embodiment two: this embodiment is a further limitation of the fiber optic gyroscope strapdown inertial navigation computer based on DSP described in specific embodiment one, and the storage module 3 includes an SD card circuit, an EEPROM circuit and a NAND Flash circuit;
[0038] The SD card circuit is used to store system data,
[0039] The EEPROM circuit is used to store solution-related data,
[0040] NAND Flash circuit is used to store control program data.
specific Embodiment approach 3
[0041]Specific embodiment three: this embodiment is a further limitation of the DSP-based fiber optic gyro strapdown inertial navigation computer described in specific embodiment one, and the communication module 4 includes a serial-to-parallel conversion module, a first RS485 / 422 bus and a second Two RS485 / 422 bus;
[0042] The GPS / log of the fiber optic gyro strapdown inertial navigation exchange data with the serial-to-parallel conversion module through the second RS485 / 422 bus;
[0043] The upper computer of the fiber optic gyro strapdown inertial navigation exchange data with the serial-to-parallel conversion module through the first RS485 / 422 bus;
[0044] The navigation solution signal input and output terminals of the serial-to-parallel conversion module are connected with the navigation solution signal input and output terminals of the DSP module 2;
[0045] The acquisition control signal output end of the serial-to-parallel conversion module is connected with the ac...
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