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unmanned aerial vehicle system introduction analysis drone cloud system control system ≥30m power system fuel engine electric motor usage time real-name registration system mushrooms gc-ms method scopethis standard collateral data elements extraction oil
MH/T 1069-2018 in English

MH/T 1069-2018 in English

VALID

Technological regulation of operation flight with unmanned aerial vehicle system

  • Issued on:2018-08-21
  • Implemented on:2018-11-01
  • File Format:PDF
  • Delivery:Via email within 5 business days
Price(USD): $330.00
$321.00


Introduction

Analysis of the core content of the standard

Element category Fixed-wing UAV Rotary-wing UAV General requirements
Take-off method Hand throwing/ejection/rolling Vertical take-off and landing Must maintain a 50m safety radius
Operating altitude Route planning altitude Control within visual range Avoid obstacles ≥30m
Power system Fuel engine Electric motor Usage time needs to be recorded

Key technical innovations

For the first time, the standard clearly defines the technical requirements for drone fences, requiring access to the drone cloud system for dynamic monitoring. For drones above 250g, a real-name registration system is implemented, and the data link system needs to have a dual redundant design.


Implementation and application suggestions

Typical scenarios: Power line inspection operations should pay special attention to the ultra-low altitude flight requirements of Article 4.3.2.6, and mountain operations need to add obstacle avoidance radar configuration. It is recommended to refer to Appendix D to establish a motor life warning mechanism.


Safety Management and Control System

The standard constructs a three-level emergency response mechanism:
1. Immediately switch to manual mode if flight control is lost within visual range (4.3.2.1)
2. Automatic return to home if contact is lost beyond visual range (7.6)
3. Execute preset forced landing if power fails (7.8)

Sample only — not a preview of MH/T 1069-2018
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