Skip to content

A Method for On-Orbit Testing of Long-Term Docking of Manned Spacecraft at the Space Station

Jul 2026 · SAE technical paper series · Vol 1 · 0 citations · 7 references

Abstract

To ensure the successful implementation of the separation, evacuation, and return processes of manned spacecraft after long-term docking at the space station, regular on-orbit health assessments must be conducted. Based on this requirement, a technical method for evaluation through autonomous on-orbit testing is proposed. First, the docking status and characteristics of the manned spacecraft’s systems, such as information management, crew environmental control, thermal control, power management, docking function, attitude, and orbit control function, are described. Then, the functional requirements for the separation, evacuation, and return of the manned spacecraft, such as the relative measurement, the relay communication, TT&C and data transmission, image and voice, instrument display and alarm, and the attitude measurement, are analyzed. Subsequently, the on-orbit testing system, test items, test procedures, and test methods for health assessment are detailed. It also provides the design of TT&C support, the design of energy support, and the main principle explanation for autonomous on-orbit testing of the system.

View source

Similar papers

Review Open access Sep 2026

The SVOM Satellite: System Design, Critical Technologies, and In-orbit Performance Assessment

The Space-based multi-band Variable Objects Monitor (SVOM) is a major Sino-French collaborative space science mission designed to detect and rapidly localize various types of gamma-ray bursts. Following its launch on 2024 June 22, the satellite successfully completed its in-orbit commissioning and verification tests by...

Dong Li, Yong-He Zhang, R. Su et al. · 0 citations
Open access Sep 2026

System-Constrained Multi-Gravity-Assist Trajectory Design for Small Satellites

Small-satellite mission design requires joint consideration of trajectory geometry, launch conditions, propulsion capacity, spacecraft mass, and operational lifetime. This study presents an integrated preliminary-design workflow combining Lambert-grid exploration, cascade filtering, and differential-evolution refinemen...

Sumeth Daluwatta, Nishanth Pushparaj · 0 citations
Conference Open access Aug 2026

Design of AUV launch and recovery system based on multi-degree-of-freedom manipulator

Aiming at the problems of high sea condition susceptibility, low automation level, and high operational risks in the storage, transportation, launching, and recovery of shipborne Autonomous Underwater Vehicles (AUVs) under complex marine wind and wave environments, this paper designs an AUV launching and recovery devic...

Jian-Li Wang, Ming-Wang Song, Xuan Qi et al. · 0 citations
Open access Nov 2026

The influence of the dynamics of an autonomous anti-aircraft system on the effectiveness of tracking and intercepting an air target

The increasing deployment of unmanned ground vehicles (UGVs) demands advanced stabilization systems capable of maintaining precise line-of-sight (LOS) target tracking under dynamic operational conditions. This paper presented a comprehensive parametric simulation framework for the preliminary design and evaluation of t...

Piotr Szmidt, Z. Koruba · 0 citations
Open access Aug 2026

Study of a Three-Claw Type Docking Mechanism with Automatic Enclosing Function for Deep Space Rendezvous and Docking

In recent years, sample returns from celestial bodies have remarkably developed as important elements of space exploration. The targets are becoming increasingly distant celestial bodies. Improving mission flexibility and reducing risk are important in deep-space exploration. The deep-space orbital transfer vehicle con...

H. Nakanishi, Akihiro Tokuyasu, Tomoharu Tanaka et al. · 0 citations

We use cookies to run the site and, with your consent, for analytics and to show ads. See our Cookie Policy.