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FG-980S Inertial Navigation System
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Introduction
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Overview
FG-980S Inertial Navigation System, in which the GNSS receiver embedded, adopts three high accuracy single-axis closed-loop miniature FOGs and quartz accelerometers. This system is compact design with very high performance as well as small size, light weight and low power consumption, which is perfectly applicable for UAV, helicopter and aircraft.
Features
• Provide self-contained, abundant, continuous and accurate navigation information
• Small size, light weight and low power consumption
• Embedded satellite navigation technology
Applications
UAVS , Helicopter , General Aviation Aircraft , etc.
Structural Dimension
Specifications
Alignment Time | GC:10min | |
Fast:5min | ||
Accuracy | Position | Inertial:1nm/h |
Integrated:20m | ||
Velocity | Inertial:1m/s | |
Integrated:0.8m/s | ||
Attitude | Inertial:0.02° | |
Integrated:0.01° | ||
Heading | Inertial:0.1° | |
Integrated:0.08° | ||
Dynamic Range | Angular Rate | ±400°/s |
Acceleration | ±15g | |
Operation Requirement | Temperature | Operating:-45~+70℃ |
Storage:-55~+85℃ | ||
Shock | Half-sinusoid:15g,11ms | |
Vibration | 0.04g2/Hz | |
MTBF | 50000h | |
Power Supply/Consumption | 28VDC/30W | |
Interface | MIL-STD-1553B | |
ARINC-429 | ||
RS-422 | ||
Dimension | Navigation unit:238mm×188mm×190mm | |
Max size:254mm×188mm×190mm | ||
Weight | 7.1kg(excluding receiving antenna) |
信息为测试元素,使用时候可删除该元素放置自己想放的元素
这里是占位文字
信息为测试元素,使用时候可删除该元素放置自己想放的元素
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