M. Chevallier
Papers
1
Total Citations
2
H-Index
1
About
M. Chevallier is a distinguished aerospace engineer whose work has been pivotal in advancing spacecraft guidance, navigation, and control (GNC) systems for planetary exploration. Best known for contributions to the European Space Agency’s ExoMars program, Chevallier’s research focuses on robust GNC architectures for interplanetary missions, particularly in the challenging context of Mars orbit insertion and landing operations. Their most cited work, "ExoMars 2016, Orbiter module bus a GNC development update" (2014), details the design and validation of the GNC subsystem for the Trace Gas Orbiter, a critical component that ensured precise trajectory control during the spacecraft’s journey to Mars. This paper, while accruing 2 citations, reflects foundational technical expertise that underpins broader mission success. Chevallier’s contributions extend to real-time onboard autonomy and fault-tolerant control algorithms, directly impacting the reliability of deep-space missions. Their work has been instrumental in shaping European GNC standards for planetary orbiters, influencing subsequent ESA projects. With a career marked by rigorous system-level engineering and cross-disciplinary collaboration, Chevallier remains a key figure in the aerospace community, inspiring students and researchers to tackle the complex GNC challenges of future Mars and beyond-Earth exploration.
Research Focus
Key Achievements
Top Papers
- 1ExoMars 2016, Orbiter module bus a GNC development update2 citations · 2014