Handling quality criterion for heading control
A heading control criterion based on the aileron-rudder sequencing required to achieve coordinated turns is presented. Quantification of the aileron-rudder shaping is obtained by consideration of the ideal crossfeed which completely eliminates sideslip induced by aileron inputs. The shaping and gain...
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| Veröffentlicht in: | Journal of aircraft 1977-02, Vol.14 (2), p.142-150 |
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| Format: | Artikel |
| Sprache: | eng |
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| container_end_page | 150 |
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| container_issue | 2 |
| container_start_page | 142 |
| container_title | Journal of aircraft |
| container_volume | 14 |
| creator | Hoh, Roger H Ashkenas, Irving L |
| description | A heading control criterion based on the aileron-rudder sequencing required to achieve coordinated turns is presented. Quantification of the aileron-rudder shaping is obtained by consideration of the ideal crossfeed which completely eliminates sideslip induced by aileron inputs. The shaping and gain parameters based on this ideal crossfeed are defined and correlated with pilot opinion ratings. Excellent correlation is obtained with data from simulation of STOL, fighter aircraft, and space shuttle vehicles. |
| doi_str_mv | 10.2514/3.44581 |
| format | Article |
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| fulltext | fulltext |
| identifier | ISSN: 0021-8669 |
| ispartof | Journal of aircraft, 1977-02, Vol.14 (2), p.142-150 |
| issn | 0021-8669 1533-3868 |
| language | eng |
| recordid | cdi_aiaa_journals_10_2514_3_44581 |
| source | Alma/SFX Local Collection |
| title | Handling quality criterion for heading control |
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