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Guidance to Control Arrival Angle and Altitude for An Unpowered Aerial Vehicle
International Journal of Aeronautical and Space Sciences ( IF 1.4 ) Pub Date : 2020-03-12 , DOI: 10.1007/s42405-020-00265-8
Seunghan Lim , Sungbong Cho , Eunyong Lee

To increase the effectiveness of a glide-bomb attack, it must be able to control the direction in which it strikes the target. Since glide bombs have different characteristics from missiles, it would not be suitable to attack at the high speed; so, it is not appropriate to use the guidance laws for the typical missiles directly. While there are many similarities with TAEM guidance for re-entry vehicle, implementation on glide bombs can degrade the performance. This paper takes into consideration the characteristics of glide bomb well and proposes a robust and straightforward guidance scheme, which is also proper for an unpowered aerial vehicle. This scheme guides the vehicle to reach the ‘target window’ controlling in the desired direction with adequate potential and kinetic energy, even in strong winds. At the end of this paper, the flight tests prove the practicality of this approach.

中文翻译:

控制无动力飞行器到达角和高度的指南

为了提高滑翔炸弹攻击的有效性,它必须能够控制它击中目标的方向。由于滑翔弹与导弹的特性不同,不适合高速攻击;因此,直接使用典型导弹的制导律是不合适的。虽然与 TAEM 再入飞行器的指导有很多相似之处,但在滑翔炸弹上的实施会降低性能。本文充分考虑了滑翔炸弹的特点,提出了一种鲁棒而直接的制导方案,该方案也适用于无动力飞行器。该方案引导车辆以足够的势能和动能控制在所需方向上的“目标窗口”,即使在强风中也是如此。在这篇论文的最后,
更新日期:2020-03-12
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