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首页> 外文期刊>Journal of Guidance, Control, and Dynamics >Comment on “Three-Dimensional Ascent Trajectory Optimization for Stratospheric Airship Platforms in the Jet Stream
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Comment on “Three-Dimensional Ascent Trajectory Optimization for Stratospheric Airship Platforms in the Jet Stream

机译:关于“射流中平流层飞艇平台的三维上升轨迹优化的评论”

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摘要

LEE and Bang [1] have recently analyzed optimal trajectories ofnan airship in the jet stream using a nonlinear point mass modelndeveloped in the relative wind frame. Using a point mass model fornthe elongated airship implies that the airship’s yawwith respect to thenrelative wind frame is always zero; i.e., the side slip angle is zero.nThis is also demonstrated by the absence of side slip in the aerody-nnamic model. For the analysis in [1] a point mass model is adequatenfor analysis because the relative heading , flight path angle u0001, andnbank angle u0002 are slowly varying such that the rotational dynamics cannsafely be ignored. Unfortunately, in forming the point mass model,nthe authors improperly consider the contribution from the addednmass of the airship. In general, the added mass should be treated as antensor in formation of the dynamics [2,3]. In [1] the tensor propertiesnof added mass are ignored and diagonal elements of the added massnmatrix are added together along with the actual mass to form a scalarntotalmassmT. In addition, the addedmass contribution is considerednproportional to the inertial velocity of the airship rather than thenrelative airspeed.
机译:LEE和Bang [1]最近使用相对风框架中开发的非线性点质量模型分析了喷气流中南飞艇的最佳轨迹。对于细长的飞艇,使用点质量模型意味着飞艇相对于相对风架的偏航始终为零;即侧滑角为零n。这也可以通过气动力学模型中没有侧滑来证明。对于[1]中的分析,点质量模型足以进行分析,因为相对航向,右航角u0001和nbank角u0002缓慢变化,从而无法安全地忽略旋转动力学。不幸的是,在建立点质量模型时,作者没有正确地考虑飞艇的附加质量的贡献。通常,在动力学形成过程中应将增加的质量视为张量[2,3]。在[1]中,附加质量的张量特性n被忽略,附加质量矩阵的对角线元素与实际质量一起被添加到一个scalarntotalmassmT中。另外,附加质量的贡献被认为与飞艇的惯性速度成正比,而不是相对于空速。

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