Attitude control of flapping wing aircraft based on energy optimization and ESO
Aiming at the problem of insufficient endurance performance of flapping wing aircraft, a stable attitude control algorithm based on energy optimization and ESO (extended state observer) is designed, which effectively reduces the energy consumption in cruise phase. Firstly, the longitudinal dynamic m...
محفوظ في:
| المؤلفون الرئيسيون: | , , |
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| التنسيق: | Artigo |
| اللغة: | Inglês |
| منشور في: |
KeAi Communications Co., Ltd.
2021-06-01
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| سلاسل: | Biomimetic Intelligence and Robotics |
| الموضوعات: | |
| الوصول للمادة أونلاين: | http://www.sciencedirect.com/science/article/pii/S266737972100005X |
| الوسوم: |
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