摘要
针对内装式机载发射运载火箭的分离方案,结合分离条件及某型号运载火箭,设计了火箭分离后的发射轨道,并研究了火箭的控制规律。分析和计算表明,所设计的发射轨道可满足卫星发射需求,所采取的控制规律切实可行,与地面发射相比,可大幅度提高运载火箭的发射能力。
With respect to the departing model of air-borne launch vehicles, a launch vehicle's trajectory is designed with departing condition and certain launch vehicle, the research on its controlling method is also done. The analysis and result indicate that its trajectory could fit the bill and the controlling method is effective. Compared with the model of launching from ground, the air-borne launch vehicle can improve its power by great extent.
出处
《飞行力学》
CSCD
北大核心
2006年第2期40-42,共3页
Flight Dynamics