Research on Agile Reentry Method for Maneuvering Vehicle

Authors

Lin Yue, 1. Beijing Institute of Control Engineering, Beijing 100094, China;;2. BUAA,7th Research Division, Beijing 100191, China;
Yingmin Jia, 2. BUAA,7th Research Division, Beijing 100191, China;
Songtao Fan, 1. Beijing Institute of Control Engineering, Beijing 100094, China;;

Abstract

Abstract: Alarge-scale orbit maneuver method is proposed and analyzed for hypersonic space reentry vehicles, and the air assisted methods are adopted to conduct space orbit maneuvers by complying with the energy balance strategy of the aircraft. By the L/D ratio of aircraft, the efficiency of the propellant use during orbital maneuvers is elevated, and the maneuverability is also enhanced, while the risk of aircraft being tracked in space can be reduced. Aero-assisted guidance technology is applied based on full-coefficient adaptive prediction-correction technology which significantly simplifies the computation of the GNC computer, while such application ensures the convergence and enhances the feasibility and comprehensive efficiency of computer. Simulation is conducted on the basis of multiple environmental conditions. The experimental results show that the proposed method significantly limits the propellant consumption in comparison with the conventional space orbit maneuvering scheme.

Recommended Citation

Yue, Lin; Jia, Yingmin; and Fan, Songtao (2021) "Research on Agile Reentry Method for Maneuvering Vehicle," Journal of System Simulation: Vol. 33: Iss. 7, Article 11.
DOI: 10.16182/j.issn1004731x.joss.20-0204E
Available at: https://dc-china-simulation.researchcommons.org/journal/vol33/iss7/11

First Page

1600

Revised Date

2020-05-07

DOI Link

https://doi.org/10.16182/j.issn1004731x.joss.20-0204E

Last Page

1608

CLC

V19;TP391

Recommended Citation

Lin Yue, Jia Yingmin, Fan Songtao. Research on Agile Reentry Method for Maneuvering Vehicle[J]. Journal of System Simulation, 2021, 33(7): 1600-1608.

DOI

10.16182/j.issn1004731x.joss.20-0204E