Position Control Design and Validation Applied to ATV During Docking to ISS

Bourdon, J.; Ganet-Schoeller, Martine; Delpy, Patrick; Ankersen, Finn

doi:10.1016/s1474-6670(17)32154-7

Cited by 3 publications

(1 citation statement)

References 2 publications

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“…The high industrialization of the approach. For example, H controllers are being used in the Ariane launcher (Mauffrey et al 1996), telecom satellites (Philippe 2011) and even in the recently operational European Automated Transfer Vehicle (ATV) (Bourdon et al 2004). In terms of H FDI, in a recent European FP7 project entitled ADDSAFE (Goupil and Marcos 2012, Marcos 2012, Henry et al 2012, and related to the application of advanced model-based techniques for commercial aircraft FDI, it was clearly shown the high potential of the technique.…”

Section: Figure 1 Basic Fdi/fdd Design Architecturementioning

confidence: 99%

Fault Detection and Isolation for a Rocket Engine Valve

Marcos

Peñín

Malikov

et al. 2013

IFAC Proceedings Volumes

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In this article a fault detection and isolation scheme based on H theory is presented for a rocket engine actuator valve. The simulation model of the engine corresponds to a Vulcain 2-like rocket engine used to study the applicability and capabilities of FDI techniques towards real-time validation in an engine test-bench. The obtained FDI design is capable of detecting and estimating (biases, ramps and including oscillatory) fault for the selected valve in a robust manner. The design methodology allows reuse of the design process for other valves with minor modifications and tuning.

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Section: Figure 1 Basic Fdi/fdd Design Architecturementioning

confidence: 99%