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Database: 365,228(8 Aug 2026)
standard control type tracking aircraft requirements target aircraft requirements time manual control system direct control dual sensor system sensor cooperation equipment ≤300ms teleoperation autonomous control control introduction analysis natural electric field method non-flex hydraulic impulse test glow discharge mass spectrometry introductionthis standard
GJB 9615.5-2019 in English

GJB 9615.5-2019 in English

VALID

Technical requirements for rendezvous and docking of manned spacecraft-Part 5:Manual control

  • Issued on:2019-12-08
  • Implemented on:2020-01-01
  • File Format:PDF
  • Delivery:Via email within 5 business days
Price(USD): $160.00
$156.00
Standard No: GJB 9615.5-2019
Document status: VALID
Title in English: Technical requirements for rendezvous and docking of manned spacecraft-Part 5:Manual control
Title in Chinese: 载人航天器交会对接技术要求 第5部分:人工控制
Language: English
File Format: Electronic (PDF)
Delivery: Via email within 5 business days
Issued on: 2019-12-08
Implemented on: 2020-01-01
Professional Classification: GJB-Military
Related Keywords: standard control type tracking aircraft requirements target aircraft requirements time
manual control system
direct control dual sensor system sensor cooperation equipment ≤300ms teleoperation
autonomous control
control introduction analysis
Related Topics: Relative value of two people
Spacecraft
China manned
Technical docking
Manned space compressor


Introduction

Analysis of the core content of the standard

Control type Tracking aircraft requirements Target aircraft requirements Time delay standard
Manned direct control Dual sensor system Sensor cooperation equipment ≤300ms
Teleoperation control Air-to-air communication system Full-function operation terminal ≤500ms

Detailed explanation of key technical requirements

3.1

The standard stipulates that the manual control system, as a hot backup system for autonomous control, needs to be configured with:

  • Rendezvous and docking sensor: image + radar dual redundant system
  • Operation equipment: separate attitude/translation control handle
  • Display device: TV image and analytical data are presented synchronously

Recommendations for the implementation of the standard

Key points of astronaut training

Based on the actual mission data of the Shenzhou spacecraft, it is recommended that:

  1. Set up 20% over-range training to deal with emergency conditions
  2. Simulator delay must be controlled within 80% of the standard value
  3. Establish an error operation database for error-proofing design optimization

Technology Evolution Analysis

Compared with the 2010 version of the standard, the main upgrades are:

  • Added ergonomic quantitative indicators for teleoperation equipment
  • Clarified the specific test method for stray light suppression of sensors
  • Refined the delay classification requirements for air-to-air communications

Sample only — not a preview of GJB 9615.5-2019
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