Exact(3)
Firstly, a functional observer is designed for the attitude systems of flexible spacecraft in order to detect the time of unknown sensor fault occurred.
Finally, the effectiveness of the proposed FTC method is demonstrated in the attitude systems of flexible spacecraft subject to a time-varying sensor fault.
In this paper, the problem of active fault tolerant control (FTC) is studied for a class of flexible spacecraft attitude systems with Lipschitz nonlinearity and sensor fault.
Similar(57)
Another attitude system requirement is a sufficient slew rate.
Within the scope of this paper, the focus will be on refinements of the Attitude system.
The Attitude system has often been applied to study interpersonal meanings in written texts.
The first stage involved the pilot study trialing the Martin and White Attitude system (2005) (which will be referred to as the 'original Attitude system' hereafter) and a thorough and critical review of the literature on the refinements of the original Attitude system.
The second process of refining the original Attitude system occurred during the application of the adapted framework to analyse the main study data, which resulted in a second set of modifications of the original Attitude system.
The Attitude system, a central element of the Appraisal framework, consists of three categories: Affect, Judgement and Appreciation (Martin and White 2005).
As briefly mentioned, the determination of the proposed refinements to the Attitude system occurred in two stages.
Similarly, Hood and Martin ([2007]) draw on the Attitude system to argue that academic writers utilised inscribed attitude in the construction of arguments within their research.
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Justyna Jupowicz-Kozak
CEO of Professional Science Editing for Scientists @ prosciediting.com