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Output details

15 - General Engineering

University of Warwick

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Output 261 of 344 in the submission

Article title

Robustness analysis of a reusable launch vehicle flight control law

Type

D - Journal article

DOI

10.1016/j.conengprac.2008.12.002

Title of journal

Control Engineering Practice

Article number

Volume number

Issue number

First page of article

751

ISSN of journal

09670661

Year of publication

2009

URL

Number of additional authors

Additional information

This paper, co-authored with industrialists from DEIMOS Space SRL in Madrid and the European Space Agency in The Netherlands, reports research funded by ESA (Contract No. 19784/06/NL/JD/na) and introduced a new optimisation-based framework for the worst-case analysis of space flight control systems. This framework was further developed over the subsequent 5 years via 8 other ESA research contracts worth a total of €485K. It has been applied to applications ranging from Autonomous Satellites, Hypersonic Re-Entry Vehicles, and Entry, Descent and Landing Systems. (Contact: Dr. Samir Bennani, Guidance, Navigation and Control Group, ESA/ESTEC, Keplerlaan 1, 2201 AZ Noordwijk, The Netherlands, samir.bennani@esa.int)

Interdisciplinary

Cross-referral requested

Research group

None

Proposed double-weighted

Double-weighted statement

Reserve for a double-weighted output

Non-English

English abstract