Aircraft Steep Approach Performance Improvements And Optimization
The present invention relates to an aircraft steep approach performance improvements and optimization, and more particularly to automatic systems and methods, which can achieve a relatively steep descent (using drag devices such as flight spoilers) at relatively low speeds while retaining good airpl...
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| Hauptverfasser: | , , |
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| Format: | Patent |
| Sprache: | chi ; eng |
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| Zusammenfassung: | The present invention relates to an aircraft steep approach performance improvements and optimization, and more particularly to automatic systems and methods, which can achieve a relatively steep descent (using drag devices such as flight spoilers) at relatively low speeds while retaining good airplane handling qualities from the pilot's point of view. |
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