University of Hertfordshire

By the same authors

An integrated Solar-Fuel Cell Powered System for Airships

Research output: Contribution to conferencePaperpeer-review

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An integrated Solar-Fuel Cell Powered System for Airships. / Khoshnoud, Farbod; Chen, Yong; Calay, Rajnish.

2012. 1066 - 1073 Paper presented at Modelling, Identification & Control (ICMIC), 2012 Proceedings of International Conference on, China.

Research output: Contribution to conferencePaperpeer-review

Harvard

Khoshnoud, F, Chen, Y & Calay, R 2012, 'An integrated Solar-Fuel Cell Powered System for Airships', Paper presented at Modelling, Identification & Control (ICMIC), 2012 Proceedings of International Conference on, China, 24/06/10 - 26/06/12 pp. 1066 - 1073 .

APA

Khoshnoud, F., Chen, Y., & Calay, R. (2012). An integrated Solar-Fuel Cell Powered System for Airships. 1066 - 1073 . Paper presented at Modelling, Identification & Control (ICMIC), 2012 Proceedings of International Conference on, China.

Vancouver

Khoshnoud F, Chen Y, Calay R. An integrated Solar-Fuel Cell Powered System for Airships. 2012. Paper presented at Modelling, Identification & Control (ICMIC), 2012 Proceedings of International Conference on, China.

Author

Khoshnoud, Farbod ; Chen, Yong ; Calay, Rajnish. / An integrated Solar-Fuel Cell Powered System for Airships. Paper presented at Modelling, Identification & Control (ICMIC), 2012 Proceedings of International Conference on, China.

Bibtex

@conference{c97f0dbae7a640e7934c7bfe83b10975,
title = "An integrated Solar-Fuel Cell Powered System for Airships",
abstract = "Development of a general model of power, propulsion and control of a novel airship is discussed in this paper. The airship design is based on the concept of the Multibody Advanced Airship for Transport (MAAT). The energy supply for this airship is produced by a solar-fuel cell system. Solar panels and fuel cells provide the power associated with the airship motion and avionics, including the control and propulsion systems. A complete model of this airship is presented by integrating the power, propulsion and control system. The model provides the base line for the design and analysis of the airship and investigation of its components, i.e. energy, control and propulsion systems and can be used in the preliminary stages of a design process.",
author = "Farbod Khoshnoud and Yong Chen and Rajnish Calay",
year = "2012",
month = jun,
language = "English",
pages = "1066 -- 1073 ",
note = "Modelling, Identification & Control (ICMIC), 2012 Proceedings of International Conference on ; Conference date: 24-06-2010 Through 26-06-2012",

}

RIS

TY - CONF

T1 - An integrated Solar-Fuel Cell Powered System for Airships

AU - Khoshnoud, Farbod

AU - Chen, Yong

AU - Calay, Rajnish

PY - 2012/6

Y1 - 2012/6

N2 - Development of a general model of power, propulsion and control of a novel airship is discussed in this paper. The airship design is based on the concept of the Multibody Advanced Airship for Transport (MAAT). The energy supply for this airship is produced by a solar-fuel cell system. Solar panels and fuel cells provide the power associated with the airship motion and avionics, including the control and propulsion systems. A complete model of this airship is presented by integrating the power, propulsion and control system. The model provides the base line for the design and analysis of the airship and investigation of its components, i.e. energy, control and propulsion systems and can be used in the preliminary stages of a design process.

AB - Development of a general model of power, propulsion and control of a novel airship is discussed in this paper. The airship design is based on the concept of the Multibody Advanced Airship for Transport (MAAT). The energy supply for this airship is produced by a solar-fuel cell system. Solar panels and fuel cells provide the power associated with the airship motion and avionics, including the control and propulsion systems. A complete model of this airship is presented by integrating the power, propulsion and control system. The model provides the base line for the design and analysis of the airship and investigation of its components, i.e. energy, control and propulsion systems and can be used in the preliminary stages of a design process.

M3 - Paper

SP - 1066

EP - 1073

T2 - Modelling, Identification & Control (ICMIC), 2012 Proceedings of International Conference on

Y2 - 24 June 2010 through 26 June 2012

ER -