孔雀垂直起降飞行器数学仿真模型  

Mathematic Model of “Peacock” Vertical Take-off and Landing Verification Platform

作　　者：贾晨辉 骆无意 柳嘉润[1] 吕新广[1] 李新明[1] 巩庆海[1] 张隽 Jia Chenhui;Luo Wuyi;Liu Jiarun;Lv Xinguang;Li Xinming;Gong Qinghai;Zhang Jun(Beijing Aerospace Automatic Control Institute,Beijing 100854,China)

机构地区：[1]北京航天自动控制研究所,宇航智能控制技术国家级重点实验室,北京100854

出　　处：《航天控制》2022年第1期17-22,共6页Aerospace Control

基　　金：国家自然科学基金(61773341)。

摘　　要：创建了“孔雀”垂直起降飞行器的数学仿真模型供飞行器控制技术人员进行可重复使用垂直起降飞行器控制技术研究。该模型包括飞行器的运动学方程、气动特性、风模型和发动机推力及伺服电机特性模型,并给出了一套模型的标称参数。本文最后采用一套制导控制策略进行了飞行器的运动仿真作为模型仿真的一套用例。A mathematical model of the vertical take-off and vertical landing aircraft for the "Peacock" aircraft is presented as a recyclable vehicle model for the research of vertical take-off and vertical landing control technology, including the aircraft′s kinematics equations, aerodynamic characteristics, wind models and engine thruster servo motor characteristic models. The nominal values of model parameters are shown. At the end of this paper, a set of guidance and control strategy is adopted to simulate the motion of the aircraft as an example of application.

关 键 词：“孔雀”飞行器 垂直起降 数学仿真模型 飞行控制仿真 

分 类 号：V19[航空宇航科学与技术—人机与环境工程]