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airborne doppler navigation systems introduction standard evolution navigation accuracy requirement horizontal straight flight test navigation computer data storage ≥100 general specification methods doppler radar speed measurement accuracy longitudinal error≤0.25 % lumber machine scopethis standard diethylene glycol indexes multi-hinged ladders
GB/T 13186-2017 in English

GB/T 13186-2017 in English

VALID

General specification for airborne Doppler navigation systems

  • Issued on:2017-12-29
  • Implemented on:2018-07-01
  • File Format:PDF
  • Delivery:Via email within 5 business days
Price(USD): $400.00
$388.00
Standard No: GB/T 13186-2017
Document status: VALID
Title in English: General specification for airborne Doppler navigation systems
Title in Chinese: 机载多普勒导航系统通用规范
Language: English
File Format: Electronic (PDF)
Delivery: Via email within 5 business days
Issued on: 2017-12-29
Implemented on: 2018-07-01
Superseding: GB/T 13186-1991 General specification for airborne doppler navigation systems
ICS Classification: 49.090-On-board equipment and instruments
Chinese Classification: M50-Radar, navigation, remote control, remote measuring and antenna synthesis
Professional Classification: GB-National Standard
Related Keywords: airborne doppler navigation systems introduction standard evolution
navigation accuracy requirement
horizontal straight flight test navigation computer data storage ≥100
general specification
methods doppler radar speed measurement accuracy longitudinal error≤0.25 %
Related Topics: Navigation System
doppler peak
Doppler
Navigation System
Doppler Velocimetry
navigation system
doppler english
GBT13186
GB/T 13186-1991
GB/T 13186-2017
doppler sensor
Phase Doppler

《GB/T 13186-2017机载多普勒导航系统通用规范》由339-1(工业和信息化部(电子))归口,主管部门为工业和信息化部(电子)。


Introduction

Standard Evolution and Technology Upgrade

GB/T 13186-2017 replaces the 1991 version of the standard. The main technical changes include: adding 9 term definitions such as hover indicator, deleting 3 obsolete terms; the navigation accuracy requirement is increased to CEP≤1.4% of the range; and the random vibration test curve (Figure 2) and software function requirements are added.


Analysis of core performance indicators

SubsystemKey parametersIndicator requirementsTest methods
Doppler radar Speed measurement accuracy Longitudinal error≤0.25%|Vt|+0.4km/h 20km horizontal straight flight test
Navigation computer Data storage ≥100 waypoints+20 route points Power-off data retention verification
Hover indicator Indication accuracy Lateral±2.5km/h Tested by special tester

Environmental adaptability requirements

Typical application scenarios: According to the classification in Appendix A, Class C2 equipment must work normally at an altitude of 10,700 meters and in an environment where the temperature is not controlled. The test must comply with the following:

  • Low temperature operation: -55℃ (Table 1)
  • Random vibration: 10-2000Hz power spectrum density 0.0005g²/Hz (Table 5)
  • Salt spray test: No corrosion for 48 hours (4.11.10)

Implementation suggestions

  1. Electromagnetic compatibility design:Requirement 4.14 requires MIL-STD-461 equivalent testing during the R&D stage
  2. Reliability verification:It is recommended to use MTBF ≥ 5000 hours as the basic indicator (4.15)
  3. Software verification:It is necessary to establish a V model development process according to GB/T 15532 (5.17)

Sample only — not a preview of GB/T 13186-2017
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