trajectory of launch vehicle

基本解釋

Simulation results show that the six-degree-of-freedom trajectory simulation model thus established can express the flight performance of the launch vehicle with accuracy.
仿真結果表明：建立的六自由度彈道仿真模型能正確反映運載火箭飛行特性；
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To research the trajectory design method for terminal area energy management(TAEM) of reusable launch vehicle(RLV), the method basing on nonlinear equations of motion is designed.
為了研究重復使用運載器末端能量管理段的下滑軌跡線設計，給出了基于高度和動壓的質點動力學的設計方法。
The system parameter design combining with the trajectory optimization design can efficiently improve the whole design performance of launch vehicle during its preliminary design.
在運載火箭概念設計階段，總體參數(shù)的確定結合軌跡優(yōu)化設計能最大程度地提高設計性能。