本文選題：復(fù)雜軌道設(shè)計(jì) + 衛(wèi)星工具包　； 參考：《空間控制技術(shù)與應(yīng)用》2016年02期

【摘要】：研究太陽帆的力學(xué)特性和軌道控制設(shè)計(jì)方法,導(dǎo)出太陽帆的無奇點(diǎn)控制律.提出通過STK中MATLAB語言編寫的嵌入式腳本(Plug-in Script)來將由控制律得到的光壓力加速度矢量,添加到STK軌道計(jì)算力學(xué)模型中,從而進(jìn)行軌道控制的方法.仿真結(jié)果表明,對(duì)于常規(guī)方法難以進(jìn)行仿真分析的航天器動(dòng)力學(xué)模型(如太陽帆),所提出的方法能快速靈活地支持其相應(yīng)的任務(wù),并增強(qiáng)任務(wù)場(chǎng)景的可視化,從而實(shí)現(xiàn)利用STK豐富的功能特性進(jìn)行復(fù)雜航天任務(wù)的設(shè)計(jì)、分析和驗(yàn)證.
[Abstract]:The mechanical characteristics of solar sail and the design method of orbit control are studied, and the control law of solar sail without singularity is derived. An embedded script (Plug-in script) written by MATLAB language in STK is proposed to add the photo-pressure acceleration vector obtained from the control law to the computational mechanics model of STK orbit, so as to carry out orbit control. The simulation results show that the proposed method can quickly and flexibly support the corresponding tasks and enhance the visualization of mission scenarios for spacecraft dynamics models (such as solar sail), which are difficult to be simulated by conventional methods. Thus, the design, analysis and verification of complex spaceflight missions can be carried out by using the rich functional characteristics of STK.
【作者單位】： 中國(guó)運(yùn)載火箭技術(shù)研究院總體設(shè)計(jì)部;中國(guó)科學(xué)院國(guó)家空間科學(xué)中心;中國(guó)空間技術(shù)研究院錢學(xué)森空間技術(shù)實(shí)驗(yàn)室;
【基金】：中國(guó)科學(xué)院戰(zhàn)略性先導(dǎo)科技專項(xiàng)資金資助項(xiàng)目(XDA04060303) 太陽帆民用航天資助項(xiàng)目
【分類號(hào)】：V442
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本文編號(hào)：1926543