MH/T 4055.3-2022 in English
VALIDTechnical specification for low altitude flight service system - Part 3: Test methods
- Issued on:2022-10-28
- Implemented on:2022-11-01
- File Format:PDF
- Delivery:Via email within 1~3 business days
$194.00
| Standard No: | MH/T 4055.3-2022 |
| Document status: | VALID |
| Title in English: | Technical specification for low altitude flight service system - Part 3: Test methods |
| Title in Chinese: | 低空飞行服务系统技术规范 第3部分:测试方法 |
| Language: | English |
| File Format: | Electronic (PDF) |
| Delivery: | Via email within 1~3 business days |
| Issued on: | 2022-10-28 |
| Implemented on: | 2022-11-01 |
| ICS Classification: | 03.220.50-Air transport |
| Chinese Classification: | V54-Air traffic control |
| Professional Classification: | MH-Civil Aviation |
| Related Keywords: | test category key indicators test method pass standard functionality
test report key test methods core test special test scenarios |
| Related Topics: | mh/t
mh/t 6027 service system low altitude low altitude aircraft Low altitude flight service system technology Low altitude flying products |
本文件规定了低空飞行服务系统的测试方法。
本文件适用于低空飞行服务系统的规划、设计、研发、建设、检验和验收。
Introduction
Standard Background and Technology Evolution
With the advancement of my country's low-altitude open policy, the general aviation field has entered a period of rapid development. As the first set of industry standards in the field of low-altitude flight services, the MH/T 4055 series of standards establishes a unified methodology for system testing in its third part. Before the formulation of this standard, the testing processes of various manufacturers had problems such as poor compatibility of ADS-B data reception and inconsistent flight plan approval processes.
Comparison of core test frameworks
| Test category | Key indicators | Test method | Pass standard |
|---|---|---|---|
| Functionality | 14 subsystem functions | Equivalence class division method | Meet MH/T 4055.2 requirements |
| Reliability | MTBF≥5000 hours | Redundancy switching test | Master-slave switching time≤30 seconds |
| Information security | Technology Protection Scheme 2.0 Level 3 | Penetration test | No high-risk vulnerabilities |
Detailed explanation of key test methods
6.1.2 Flight plan processing
Use the boundary value analysis method to verify the required fields:
- Aircraft registration number: Test the abnormal situation containing special characters (such as B-123*)
- Planned take-off time: Verify the cross-date boundary processing (23:59→00:01)
6.1.3 Surveillance data processing
Focus on testing the ADS-B track fusion algorithm:
- When there is a conflict in multi-source data, 1090ES signal is given priority
- Track update delay should be ≤2 seconds (under 4G communication environment)
Implementation suggestions
Test environment establishment
It is recommended to adopt a three-level architecture simulation environment:
- National level: Deploy a virtualization platform to simulate multi-regional data collection
- Regional level: Configure at least 2 redundant servers
- Service station level: Must include actual self-observing meteorological equipment access
Document management
The test report must include:
- Original data records of all test cases
- Network topology diagram for performance testing
- Vulnerability scanning report for security testing
Technology evolution direction
This standard may be supplemented in the future:
- 5G-AeroMACS communication test requirements
- Special test scenarios for UAV beyond visual line of sight (BVLOS) operations
- AI-based trajectory prediction algorithm verification specifications

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