Scholarlink

The conceptual design and initial sizing may be combined and be referred to as the preliminary design phase. Four fundamental UAV parameters are determined during the preliminary design phase: 1. UAV Configuration, 2. UAV maximum take-off weight (WTO), 3. Wing reference area (S), and 4. Engine thrust (T) or engine power (P). These four parameters will govern the UAV size, the manufacturing cost, and the complexity of calculation. In this chapter, design activities in conceptual design and initial sizing are provided.

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

Preliminary Design

  • 章节

  • 发表日期：

    2025年

查看全文
  • Mohammad H. Sadraey

摘要

The conceptual design and initial sizing may be combined and be referred to as the preliminary design phase. Four fundamental UAV parameters are determined during the preliminary design phase: 1. UAV Configuration, 2. UAV maximum take-off weight (WTO), 3. Wing reference area (S), and 4. Engine thrust (T) or engine power (P). These four parameters will govern the UAV size, the manufacturing cost, and the complexity of calculation. In this chapter, design activities in conceptual design and initial sizing are provided.