Based on the primary principle of flight dynamics, the paper studies the flight quality of Tailless Flying-wing HALE UAV and Taill Flying-wing according to traditional calculation methods.
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- 本論文以經(jīng)典飛行動(dòng)力學(xué)原理為基礎，利用傳統的飛行力學(xué)計算分析方法，對飛翼布局的高空長(cháng)航時(shí)無(wú)人機的飛行品質(zhì)與有尾飛翼布局和常規布局的飛行品質(zhì)進(jìn)行了對比研究。
