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Energy Optimal Spacecraft Attitude Control Subject To Convergence Rate Constraints

Horri, NM, Palmer, P and Roberts, M (2011) Energy Optimal Spacecraft Attitude Control Subject To Convergence Rate Constraints Control Engineering Practice, 19 (11). pp. 1297-1314.

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Item Type: Article
Divisions : Faculty of Engineering and Physical Sciences > Electronic Engineering > Surrey Space Centre
Authors :
AuthorsEmailORCID
Horri, NMUNSPECIFIEDUNSPECIFIED
Palmer, PUNSPECIFIEDUNSPECIFIED
Roberts, MUNSPECIFIEDUNSPECIFIED
Date : November 2011
Identification Number : https://doi.org/10.1016/j.conengprac.2011.07.002
Depositing User : Symplectic Elements
Date Deposited : 28 Mar 2017 14:59
Last Modified : 28 Mar 2017 14:59
URI: http://epubs.surrey.ac.uk/id/eprint/26840

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