CAJ | 학술논문

飞艇载荷能力会随着大气环境因素和飞艇自身飞行状况的变化而变化，为了找出这种变化规律，对飞艇载荷能力的影响因素进行研究。首先分析飞艇在飞行过程中处于平衡状态下的受力情况，得出对飞艇载荷能力的各种影响因素，而后通过进一步的理论分析，在一定的假设前提下，建立飞艇受力的数学模型，并利用Matlab软件进行仿真分析，给出飞艇载荷能力与大气环境、飞行情况、初始充入氦气情况、起飞高度之间的数值变化关系。该研究可为飞艇的使用提供借鉴和理论依据。
비정재하능력회수착대기배경인소화비정자신비행상황적변화이변화，위료조출저충변화규률，대비정재하능력적영향인소진행연구。수선분석비정재비행과정중처우평형상태하적수력정황，득출대비정재하능력적각충영향인소，이후통과진일보적이론분석，재일정적가설전제하，건립비정수력적수학모형，병이용Matlab연건진행방진분석，급출비정재하능력여대기배경、비행정황、초시충입양기정황、기비고도지간적수치변화관계。해연구가위비정적사용제공차감화이론의거。
In order to find rules that load capacity of airship varies with atmosphere environment and flight status of airship, research affecting factors for load capacity of airship. First the endured forces of conventional airship under equilibrium condition were analyzed. And affecting factors for load capacity of airship were gained. Through further theoretical analysis, force mathematical model of airship was established basing on certain assumptions and simulations were carried out with Matlab software platform. Relationship of value changes between load capacity of airship and atmosphere environment, flight conditions, the initial conditions of charging into helium, taking off height were given, which making itself a theoretical basis for the use of airship.