Satellite inertial navigation combined type missile guidance control system and simulation method
The invention discloses a satellite inertial navigation combined type missile guidance control system, and relates to the technical field of forest fire control, the control system is based on a frame structure of a digital signal processor DSP and a programmable logic device FPGA, and the control s...
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Format: | Patent |
Sprache: | chi ; eng |
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Zusammenfassung: | The invention discloses a satellite inertial navigation combined type missile guidance control system, and relates to the technical field of forest fire control, the control system is based on a frame structure of a digital signal processor DSP and a programmable logic device FPGA, and the control system comprises a control panel, a main controller arranged on the control panel, a power supply module, a function module, an IMU module, a GNSS receiving module, an interface module and a shell; the control system adopts the combined guidance of an IMU module and a GNSS receiving module. The invention further provides a simulation method of the satellite inertial navigation combined type missile guidance control system. According to the invention, the actual urgent need of insufficient accurate putting capability of forest remote guidance fire extinguishing equipment can be solved, the blank of large-scale production of fire extinguishing bomb flight control equipment is filled up, and an important position is oc |
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