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Autonomous mission reconstruction during the ascending flight of launch vehicles under typical propulsion system failures
作者姓名:Zhengyu SONG  Yin LIU  Yong HE  Cong WANG
作者单位:1. China Academy of Launch Vehicle Technology;2. Beijing Institute of Astronautical Systems Engineering;3. Beijing Aerospace Automatic Control Institute
基金项目:the National Natural Science Foundation of China (No. 61773341);
摘    要:In recent years, Chinese Long March(LM) launchers have experienced several launch failures, most of which occurred in their propulsion systems, and this paper studies Autonomous Mission Reconstruction(AMRC) technology to alleviate losses due to these failures. The status of the techniques related to AMRC, including trajectory and mission planning, guidance methods,and fault tolerant technologies, are reviewed, and their features are compared, which reflect the challenges faced by AMRC technology...

收稿时间:10 November 2020

Autonomous mission reconstruction during the ascending flight of launch vehicles under typical propulsion system failures
Zhengyu SONG,Yin LIU,Yong HE,Cong WANG.Autonomous mission reconstruction during the ascending flight of launch vehicles under typical propulsion system failures[J].Chinese Journal of Aeronautics,2022,35(6):211-225.
Institution:1. China Academy of Launch Vehicle Technology, Beijing 100076, China;2. Beijing Institute of Astronautical Systems Engineering, Beijing 100076, China;3. Beijing Aerospace Automatic Control Institute, Beijing 100854, China
Abstract:In recent years, Chinese Long March (LM) launchers have experienced several launch failures, most of which occurred in their propulsion systems, and this paper studies Autonomous Mission Reconstruction (AMRC) technology to alleviate losses due to these failures. The status of the techniques related to AMRC, including trajectory and mission planning, guidance methods, and fault tolerant technologies, are reviewed, and their features are compared, which reflect the challenges faced by AMRC technology. After a brief introduction about the failure modes of engines that can occur during flight, and the fundamentals of trajectory planning and joint optimization of the target orbit and flight path, an AMRC algorithm is proposed for geostationary transfer orbit launch missions. The algorithm evaluates the residual performance onboard, and plans new objectives and corresponding flight path by iterative guidance mode or segmented state triggered optimization methods in real-time. Three failure scenarios that have occurred during previous LM missions are simulated to check the robustness of the algorithm: imminent explosion risk of the boosters’ engines, thrust drop during the first stage of flight, and being unable to start the engine during the second stage. The payloads would fall from space according to the current design under these conditions, but they were saved with the AMRC algorithm in the simulations, which allowed the rocket to get into the target orbit as intended or the payloads were deployed in other orbits without crashing. Although spaceflight can be very unforgiving, the AMRC algorithm has the potential to avoid the total loss of a launch mission when faced with these kinds of typical failures.
Keywords:Autonomous mission reconstruction  Closed-loop guidance  State triggered indices  Rescue orbits  Launch vehicles
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