| 摘要 |
<p>A kite is disclosed. The kite comprises a first control element coupled to the kite in a first tether-force configuration, wherein the first control element is used to maintain controlled flight of the kite in the first tether- force configuration during a power generating phase. The kite further comprises a second control element coupled to the kite in a second tether-force configuration, wherein the second control element is used to maintain controlled flight of the kite in the second tether-force configuration during a recovery phase, and wherein during the recovery phase a tether force associated with the second tether-force configuration is reduced as compared to the tether force associated with the first tether-force configuration during the power generating phase</p> |
