Lateral Directional Aircraft Control Using Eigenstructure Assignment
A state-space model of desired aircraft lateral-directional responses based on flying quality specifications is here used to generate the eigenvalues and eigenvectors that are to be obtained by means of feedback control. A direct method is used to calculate the gain matrix, which achieves the desire...
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| Veröffentlicht in: | Journal of guidance, control, and dynamics control, and dynamics, 1998-05, Vol.21 (3), p.523-525 |
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| Format: | Artikel |
| Sprache: | eng |
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| Online-Zugang: | Volltext |
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| Zusammenfassung: | A state-space model of desired aircraft lateral-directional responses based on flying quality specifications is here used to generate the eigenvalues and eigenvectors that are to be obtained by means of feedback control. A direct method is used to calculate the gain matrix, which achieves the desired eigenvalues exactly and the desired eigenvectors in a best least-squares sense. (AIAA) |
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| ISSN: | 0731-5090 1533-3884 |
| DOI: | 10.2514/2.7612 |