一类平流层飞艇质量和惯量特性的计算方法与分析  

Calculation and Analysis for Mass and Inertia Characteristics of a Class of Stratospheric Airship

作　　者：吴雷[1,2] 李勇[3] 李智斌[1,2] 

机构地区：[1]北京控制工程研究所,北京100190 [2]空间智能控制技术重点实验室,北京100190 [3]中国空间技术研究院,北京100094

出　　处：《空间控制技术与应用》2010年第6期39-42,共4页Aerospace Control and Application

基　　金：国家自然科学基金(11072028)资助项目

摘　　要：针对一类具有双拼椭球体外形的平流层飞艇,根据适当假设,给出该类飞艇质量和惯量特性的解析计算方法.以飞艇上升过程为例,通过仿真计算给出该过程飞艇质量、质心位置和转动惯量的变化曲线,结合理论分析,验证该计算方法的合理性.最后,简要分析了质量和惯量特性变化对飞艇运动稳定性和能控性的影响.In this paper,an analytic calculation method for mass and inertia characteristics of a class of stratospheric airship with double semi-ellipsoid shape is proposed according to proper assumptions.Variation curves of airship＇s mass,position of mass center and inertia are given by simulating airship＇s rising process.The rationality of this method is demonstrated based on theoretical analysis.At last,the influence of the airship＇s mass and inertia characteristics on its stability and controllability are briefly analyzed.

关 键 词：平流层飞艇 双拼椭球体 质量和惯量 

分 类 号：V448[航空宇航科学与技术—飞行器设计]