A generic method for robust performance analysis of aircraft DC power systems

Sautreuil, Matthieu; Rétière, Nicolas; Riu, Delphine; Sename, Olivier

doi:10.1109/iecon.2008.4757928

Cited by 9 publications

(16 citation statements)

References 4 publications

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“…At this step of the design process, an optimal close loop device has been designed from a weight point of view. But to ease the integration into the DC system, the authors suggested in [3] to impose to the device suppliers that the subsystems must be robust to DC side uncertainties. This is the third step of the design process.…”

Section: Feedback 2 Feedbackmentioning

confidence: 99%

“…5. The background for computing µ and its application to aircraft system robust performance analysis is presented in [3]. According to the different configurations (Fig.…”

Section: µ-Analysismentioning

confidence: 99%

“…For parametric uncertainties, the model structure is known but the q p parameters are uncertain. They are expressed by [3]:…”

Section: Modeling Uncertaintiesmentioning

confidence: 99%

“…The robust analysis methods are based upon the calculation of structured singular values µ [3]. System uncertainties modeling is added to the general control configuration in Fig.…”

Section: µ-Analysismentioning

confidence: 99%

“…On-board aircraft electrical power system is then set to evolve, with the "All Electrical" concept, to a High Voltage DC structure, mainly for weight gain, efficiency, reliability and reduced maintenance cost reasons [1]. This evolution was initiated by the European aircraft manufacturers in the "Power Optimized Aircraft" EU project and is now followed by the "More Open Electrical Technologies" project [2,3,4]. To achieve efficient operation conditions, several standards are imposed by the aircraft manufacturer to the individual devices suppliers.…”

Section: Introductionmentioning

confidence: 99%

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A new methodology for aircraft HVDC power systems design

Hernández¹,

Sautreuil²,

Rétière³

et al. 2009

2009 IEEE International Conference on Industrial Technology

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-A new methodology for aircraft HVDC power systems design is first proposed. The first goal is to design the network subsystems in order to obtain optimal devices from a weight point of view. The contribution of optimal linear multivariable control methods is shown to be major for this first design objective and H 8 synthesis is applied in this paper. The second design objective is that the devices exhibit an adequate dynamical behavior when integrated into the DC network. But during design phases, the aircraft subsystems providers generally do not know the parameters of the DC network. To guarantee an easy integration of the subsystems, the device design should be robust to DC network uncertainties. Robust performance analysis method is applied in this paper and is integrated in the proposed methodology.

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Section: Feedback 2 Feedbackmentioning

confidence: 99%

“…5. The background for computing µ and its application to aircraft system robust performance analysis is presented in [3]. According to the different configurations (Fig.…”

Section: µ-Analysismentioning

confidence: 99%

“…For parametric uncertainties, the model structure is known but the q p parameters are uncertain. They are expressed by [3]:…”

Section: Modeling Uncertaintiesmentioning

confidence: 99%

“…The robust analysis methods are based upon the calculation of structured singular values µ [3]. System uncertainties modeling is added to the general control configuration in Fig.…”

Section: µ-Analysismentioning

confidence: 99%

Section: Introductionmentioning

confidence: 99%

See 3 more Smart Citations

A new methodology for aircraft HVDC power systems design

Hernández¹,

Sautreuil²,

Rétière³

et al. 2009

2009 IEEE International Conference on Industrial Technology

Self Cite

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The Robustness: A New Approach for the Integration of Energetic Systems

Rétière¹,

Riu²,

Sautreuil³

et al. 2012

Systemic Design Methodologies for Electrical Energy Systems

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Stability enhancement in DC distribution systems with constant power controlled converters

Grillo

Musolino²,

Sulligoi

et al. 2012

2012 IEEE 15th International Conference on Harmonics and Quality of Power

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DC distribution is becoming more and more a suitable technical solution for medium voltage (MV) distribution systems especially in presence of storage devices and renewable energy sources. Among the different challenging issues concerning the new topological configurations of DC systems, stability represents a topic of paramount importance. The paper presents, by means of numerical continuation method, the stability analysis of two DC distribution systems which supply constant power loads (CPLs) connected to the AC grid with an interface converter. CPLs behavior may provoke voltage instability of the DC systems. The paper presents the approach used to maximize, by means of a feedback action on the interface converter, the stable region of operation of the DC distribution systems

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A generic method for robust performance analysis of aircraft DC power systems

Cited by 9 publications

References 4 publications

A new methodology for aircraft HVDC power systems design

A new methodology for aircraft HVDC power systems design

The Robustness: A New Approach for the Integration of Energetic Systems

Stability enhancement in DC distribution systems with constant power controlled converters

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