发明名称 LENTICULAR AIRSHIP AND ASSOCIATED CONTROLS
摘要 A system for controlling yaw associated with an airship may include one or more vertical control surfaces associated with the airship, a first power source and a second power source, each configured to provide a thrust associated with the airship, and a yaw control configured to receive an input indicative of a desired yaw angle. The system may further include a controller communicatively connected to the yaw control, the one or more vertical control surfaces, and the first and second power sources. The controller may be configured to receive an output signal from the yaw control corresponding to the desired yaw angle and to generate a control signal configured to modify a state associated with at least one of the one or more vertical control surfaces, the first power source, and the second power source, such that the airship substantially attains the desired yaw angle.
申请公布号 US2013043353(A1) 申请公布日期 2013.02.21
申请号 US201213649177 申请日期 2012.10.11
申请人 LTA CORPORATION;LTA CORPORATION 发明人 BALASKOVIC PIERRE
分类号 B64C13/16;B64B1/00;B64C9/00;B64C13/04;B64C19/00 主分类号 B64C13/16
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