Optimization of Spacecraft Thrusters Configuration Under Fault Diagnosability and Recoverability Constraints

Author:

Faure Martin1ORCID,Henry David1ORCID,Cieslak Jerome1ORCID,Lachevre Pierre2,Ankersen Finn3

Affiliation:

1. IMS Lab., University of Bordeaux, Bordeaux INP, CNRS (UMR 5218), 351 cours de la liberation, Talence cedex, France

2. Airbus Defence and Space SAS, 31 rue des Cosmonautes, France

3. ESA/ESTEC, Keplerlaan 1, 2201 AZ Noordwijk, Netherlands

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Subject

Electrical and Electronic Engineering,Aerospace Engineering

Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Optimized Digital Simulation Methodology for System Validation Using Real-Time Hardware-in-Loop Simulation Platform;IEEE Aerospace and Electronic Systems Magazine;2024-08

2. A Data-Driven Fault Detectability Analysis Approach Based on Actuator and Sensor Performance;2024 9th International Conference on Automation, Control and Robotics Engineering (CACRE);2024-07-18

3. A Design Method for Redundant Microthruster Layout With Allocation Error;International Journal of Aerospace Engineering;2024-01

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