Scholarlink

The article addresses the development of an automatic take-off and landing (ATOL) framework for a self-propelled, fixed-wing, tethered aircraft. The ATOL is performed with a circular trajectory defined by the tether length and the central anchorage point. A control architecture for ATOL is proposed, with controllers designed for each flight phase, focusing on the variable tether length during the ascending mode. The simulation shows promising results, with the kite being able to elevate and increase the tether length. These developments are intended for use in an Airborne Wind Energy System.

错误：搜索内容不能为空，请输入英文关键词
错误：关键词超出字数限制，请精简
高级检索

Circular Take-Off and Landing of Tethered Aircraft with Variable Tether Length

  • 会议论文

  • 发表日期：

    2025年

查看全文
  • Sérgio Vinha,
  • Gabriel M. Fernandes,
  • Fernando A.C.C. Fontes

摘要

The article addresses the development of an automatic take-off and landing (ATOL) framework for a self-propelled, fixed-wing, tethered aircraft. The ATOL is performed with a circular trajectory defined by the tether length and the central anchorage point. A control architecture for ATOL is proposed, with controllers designed for each flight phase, focusing on the variable tether length during the ascending mode. The simulation shows promising results, with the kite being able to elevate and increase the tether length. These developments are intended for use in an Airborne Wind Energy System.