supported by National Natural Science Foundation of China(Grant Nos.12202068,12202087);China National Space Administration Preliminary Research Project(Grant Nos.KJSP2023020201,KJSP2020010402).
It is widely known that the hypervelocity impact of orbital debris can cause serious damage to spacecraft,and enhancing the impact resistance is the great concern of spacecraft shield design.This paper provides a comp...
supported by the National Natural Science Foundation of China under Grant No.12072090.
The high-speed development of space defense technology demands a high state estimation capacity for spacecraft tracking methods.However,reentry flight is accompanied by complex flight environments,which brings to the ...
Spacecraft trajectory optimization is essential for all the different phases of a space mission,from its launch to end-of-life disposal.Due to the increase in the number of satellites and future space missions beyond ...
supported by the National Key R&D Program of China(No.2020YFC2201200).
Configuration stability is essential for a space-based Gravitational-Wave(GW)observatory,which can be impacted by orbit insertion uncertainties.Configuration uncertainty propagation is vital for investigating the infl...
supported by National Natural Science Foundation of China (Nos. 51937004 and 51977002);sponsored by Beijing Nova Program (No. 20220484153)。
In the space plasma environment, primary discharge may occur on the solar array and evolve into a destructive sustained arc, which threatens the safe operation of the spacecraft. Based on the plasma expansion fluid th...
supported by the National Natural Science Foundation of China(Nos.62371375,62371372,62101406 and 62001340);Innovation Capability Support Program of Shaanxi,China(No.2022TD-37);the Fundamental Research Funds for Central Universities,China(Nos.XJS221302 and QTZX23060).
The Tracking,Telemetering,and Command(TT&C)communication of spacecraft faces severe limitations during reentry.The Electromagnetic(EM)propagation channel is influenced by changes in the flight state and fluid dynamics...
funded by the National Key Research and Development Program of China (2020YFB0505804);National Natural Science Foundation of China (Grant Nos.42388102 and 42204015);Natural Science Foundation of Shandong Province (ZR2022QD094).
Global Navigation Satellite System(GNSS)can provide an approach for spacecraft autonomous navigation in earth-moon space to make up for the insufficiency of earth-based tracking,telemetry,and control systems.However,i...
National Science Foundation of China(Grant No.:52206113);Science Fund Program for Distinguished Young Scholars(Overseas)(Grant No.:GYKP020).
Due to the rapid development of the space industry,ever higher demands are being made for the optimization and improvement of spacecraft thermal management systems.Thermal control technology has become one of the key ...
Supported by the Strategic Priority Research Program of the Chinese Academy of Sciences(XDB0560000,XDA15320000);the National Key R&D Program of China(2022 YFF0503002);the National Natural Science Foundation of China(12233012,12333010,11921003)。
The Advanced Space-based Solar Observatory(ASO-S)marked China's first comprehensive solar mission in space.Drawing upon the previous reports covering 2018-2020 and 2020-2022,we present here an update on the ASO-S made...
This work was supported by the National Key Research and Development Program of China(2021YFB2900603);the National Natural Science Foundation of China(61831008).
A dynamic multi-beam resource allocation algorithm for large low Earth orbit(LEO)constellation based on on-board distributed computing is proposed in this paper.The allocation is a combinatorial optimization process u...