滑翔机动态轨迹控制
Dynamic trajectory control of gliders
摘要：
提出了一种新的动力学控制算法，以引导滑翔机的轨迹到预先指定的目标点。算法迭代运行，并且到目标点的方法是自我校正的。该算法适用于在行星大气中行驶的任何无动力升力使能飞行器（滑翔机）。作为一个概念的证明，我们已经应用了新的算法的命令和控制的轨迹的航天飞机在终端区域能量管理（TAEM）阶段。
英文摘要：
A new dynamic control algorithm in order to direct the trajectory of a glider to a pre-assigned target point is proposed. The algorithms runs iteratively and the approach to the target point is self-correcting. The algorithm is applicable to any non-powered lift-enabled vehicle (glider) travelling in planetary atmospheres. As a proof of concept, we have applied the new algorithm to the command and control of the trajectory of the Space Shuttle during the Terminal Area Energy Management (TAEM) phase.
机构、总结、中文摘要均由AI分析而来，可能存在错误，请以论文正文为准。
