带内稳定性的垂直起降飞机的部分线性化

52nd IEEE Conference on Decision and Control Pub Date : 2013-12-09 DOI:10.1109/CDC.2013.6760268

Vincent Léchappé, Y. Aoustin, Luis Alejandro Marquez Martinez, C. Moog

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引用次数: 3

摘要

通过对各种反馈线性化解的检验，求解了平面垂直起降飞机。对状态空间进行部分线性化，保证了相关内部动力学的稳定性。通过寻找具有稳定的0维、1维或2维零动力学的虚拟输出得到结果。

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Partial linearization of the PVTOL aircraft with internal stability

The planar vertical take-off and landing (PVTOL) aircraft is worked out by inspecting the various feedback linearization solutions. Partial linearizations of the state space are performed, which ensure the stability of the associated internal dynamics. The results are obtained through the search of dummy outputs with a 0-dimensional, 1-dimensional or 2-dimensional zero-dynamics that are stable.

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52nd IEEE Conference on Decision and Control

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