| 产品>>惯性产品>>捷联惯性导航系统 |
| 捷联惯性导航系统 |
| 捷联惯性导航系统 Model: SINS500 |
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捷联惯性导航系统是以光纤陀螺，精密的加速度计和插件式计算机为基础，组合了GPS/GLONASS接收机。
光纤捷联惯性导航系统具有完全的固态设计，无旋转或其他可动部件。由于她没有可动部件，因此不要求重新校准完全免维护。这些系统有很高的可靠性（MTBF），在其寿命期内不要求维护。模拟和数字显示单元和其他外围设备通过串行接口提供输出数据。捷联惯性导航系统，设计用于随车携带的船舰和海底交通工具，是紧凑，坚固，免维护和低消耗的设备。 |
| 捷联惯性导航系统 Model: SINS1000 |
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捷联惯性导航系统是以光纤陀螺，精密的加速度计和插件式计算机为基础，组合了GPS/GLONASS接收机。
光纤捷联惯性导航系统具有完全的固态设计，无旋转或其他可动部件。由于她没有可动部件，因此不要求重新校准完全免维护。这些系统有很高的可靠性（MTBF），在其寿命期内不要求维护。模拟和数字显示单元和其他外围设备通过串行接口提供输出数据。捷联惯性导航系统，设计用于随车携带的船舰和海底交通工具，是紧凑，坚固，免维护和低消耗的设备。 |
| 低价位惯性和GPS组合导航系统 Model: RT2000 |
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RT2000系列产品是测量运动、位置、和方向的高级、精密的惯性和GPS导航系统。
RT2000系列产品使用惯性导航系统技术并将惯性导航同GPS接收机组合在一起。惯性导航和GPS最好的特性被组合在一起给出了一最优的解决方案。
系统在市区或树木覆盖的环境中通过提供精确的速度提高了单纯GPS系统的性能。对于传统垂直参考单元或稳定平台所共有的漂移被自动修正以使RT2000系列产品能够没有漂移或不需重置而长时间工作。
选择合适的RT2000系列产品
在RT2000系列中有四款产品。RT2500和RT2502产品数据更新率达到100Hz。RT2500-250和RT2502-250数据更新率达到250Hz。RT2500和RT2500-250更适合用在公路上，当高速移动时能够保持精确的方向。RT2502和RT2502-250是双天线型能够在所有车辆所有速度运行时保持精确的方向。 |
| 惯性和GPS组合导航系统 Model: RT3000 |
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RT3000系列产品是高级精密的惯性和GPS导航系统，用于测量物体运动，位置和方向。系统使用惯性导航系统技术并将其同高质量测量级GPS接收机组合在一起，协调了惯性导航系统和GPS的最优特性以提供最优解决方案。
系统通过在城市或有树木覆盖的环境中提供精确的速度提高了只有GPS的系统的性能。在传统的垂直参考单元（VRU）或稳定平台中常见的漂移被自动改正，因此RT3000系列产品可无限期使用，没有漂移或不需要重置。 |
| 惯性和GPS组合导航系统 Model: RT4000 |
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RT4000系列产品是在高速时（250Hz）测量运动、位置、和方向的高级、精密的惯性和GPS导航系统。
RT4000系列产品使用惯性导航系统技术并将惯性导航同最高质量的测量级GPS接收机组合在一起。惯性导航和GPS最好的特性被组合在一起给出了一最优的解决方案。
系统在市区或树木覆盖的环境中通过提供精确的速度提高了单纯GPS系统的性能。对于传统垂直参考单元或稳定平台所共有的漂移被自动修正以使RT4000系列产品能够没有漂移或不需重置而长时间工作。
选择合适的RT4000系列产品
RT4000系列的成员之间主要区别是测量的精确度。所有成员使用相同的的处理平台、外壳、电缆连接线等。工作温度、供应电压和尺寸规格都是相同的或相似的。 |
| 垂直参考单元 Model: iNAV-FMS-VRU |
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iMAR's vertical reference unit iNAV-FMS-VRU is
a derivation of iMAR's well-known inertial measurement
system iNAV-FMS for inertial control,
stabilization, guidance, tracking and dynamic
analysis, which is equipped with high precision
multiplexed closed-loop
fiber optical gyros and
servo-accelerometers
and covers applications
which require high accuracy,
reliability and an
open interface.
The system provides
interfaces for speed
measurement (counter
input or EM-Log/DVL via
RS232/422) and GPS
(embedded or external).
Possible data outputs
are RS232, CAN,
Ethernet or/and analog output (synchro on request).
Special adaptation of housing and mechanical
dimensions is possible. Data processing
(strap-down algorithms, attitude and heading
calculation, dead-reckoning navigation, aiding
with external heading information and heading
bandwidth improvement) inside of the measuring
system is as well possible as data transmission
of pure or corrected raw data. |
| 垂直参考单元 Model: iVRU-FC-FF |
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With iVRU-FC-C167 a vertical reference unit is provided
for applications which require
high accuracy and simple using.
iVRU-FC is a triaxial system with three
orthogonal mounted rugged fiber optic
gyroscopes, three ultra ruggedised
MEMS accelerometers and an integrated
powerful micro-processor with
16 bit sensor data digitalisation to provide digital
data transmission (CAN,
RS232) and extended internal
error modelling. As an
option also analog output
data can be provided. As a
further option an internal
GPS / magnetometer can be
provided as well as a speed
sensor interface to achieve
higher performance also in
difficult environment. Interfaces
for platform stabilisation
are available on request.
Qualification according to
MIL-STD-810F and MILSTD-
461E possible on request
(iVRU-FC-M). |
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| 惯性测量系统（雷达/大地测量应用） Model: iNAV-FMS-LSURV |
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iNAV-FMS is an IMS product family for inertial
navigation and guidance, stabilisation, heading
determination and dynamically motion analysis
with fiber optical gyros that covers applications,
which require high accuracy, reliability and an
open interface to the user.
The derivation iNAV-FMS-LSURV for advanced
land vehicle based applications consists of three
high accurate fiber optical gyroscopes with low
random walk of 0.18 deg/ h and angular resolution
of 0.0003 deg, three servo accelerometers,
a powerful strapdown processor and an open
and flexible interface, which can be customized.
As an option the modular designed system provides
interfaces to (D)GPS/GLONASS, external
trigger input/output and external I/Os for e.g. laser
ranger, camera platform control, stabilisation
and synchronisation. Possible outputs are
Ethernet (TCP/IP or UDP), RS232/422 or internal
data storage on the integrated 4 GByte silicondisk. |
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| 惯性测量系统（航空应用） Model: iNAV-FMS-AIRSURV |
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iNAV-FMS is an IMS product family for inertial
navigation and guidance, stabilisation, true
heading determination and dynamically motion
analysis with fiber optical gyros that covers applications,
which require high accuracy, reliability
and an open interface to the user.
The derivation iNAV-FNS-AIRSURV for advanced
airborne applications consists of three
high accurate fiber optical gyroscopes with low
random walk of 0.10 deg/ h and angular resolution
of 0.0003 deg, three servo accelerometers,
a powerful strapdown processor and an open
and flexible interface, which can be customized.
As an option the modular designed system provides
interfaces to (D)GPS/GLONASS, external
trigger input/output and external I/Os for e.g. laser
altimeter, SAR or camera platform control,
stabilisation and synchronisation. Possible outputs
are Ethernet (TCP/IP or UDP), RS232/422
or analog as well as internal data storage on silicondisk. Furthermore application specific interfaces
can be realized on request (e.g. ARINC
429). |
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