| 摘要 |
An unmanned flying vehicle comprises an autonomous flying wing (10) having at least two wing portions (14, 16) arranged substantially symmetrically about a center portion (12). Each wing portion is pivotally attached to each adjoining portion such that the wing portions are foldable for storage and openable for deployment. A preferred form is the so-called seagull wing having four wing portions. The vehicles may be programmable from a mother aircraft whilst being borne to a deployment zone using a data link which may be wireless. |
