导弹与航天运载技术
導彈與航天運載技術
도탄여항천운재기술
MISSILES AND SPACE VEHICLES
2015年
1期
38-41
,共4页
魏洪亮%陆宏志%赵静%徐志程%裴胤
魏洪亮%陸宏誌%趙靜%徐誌程%裴胤
위홍량%륙굉지%조정%서지정%배윤
水下垂直发射%弹性体%环境载荷%水弹道
水下垂直髮射%彈性體%環境載荷%水彈道
수하수직발사%탄성체%배경재하%수탄도
Vertical sub-launching%Elastic body%Environmental loads%Water trajectory
考虑水下航行体的弹性特性，建立航行体与发射筒之间接触、摩擦作用的刚柔耦合模型，发展了多约束航行体水下垂直发射动力学仿真分析方法。给出算例，获得了筒内弹道、水中弹道、航行体姿态和内部载荷等参数的变化规律。分析表明，计算结果能够反映航行体水下垂直发射过程的特点，计算方法合理可行。
攷慮水下航行體的彈性特性，建立航行體與髮射筒之間接觸、摩抆作用的剛柔耦閤模型，髮展瞭多約束航行體水下垂直髮射動力學倣真分析方法。給齣算例，穫得瞭筒內彈道、水中彈道、航行體姿態和內部載荷等參數的變化規律。分析錶明，計算結果能夠反映航行體水下垂直髮射過程的特點，計算方法閤理可行。
고필수하항행체적탄성특성，건립항행체여발사통지간접촉、마찰작용적강유우합모형，발전료다약속항행체수하수직발사동역학방진분석방법。급출산례，획득료통내탄도、수중탄도、항행체자태화내부재하등삼수적변화규률。분석표명，계산결과능구반영항행체수하수직발사과정적특점，계산방법합리가행。
A rigid-flexible coupled model considering contact and friction between underwater vehicle and launching tube was proposed, and dynamic simulation method for vertical sub-launching process of multiple constraints elastic body was established. The results of calculation example are introduced, which contain the varying rules of parameters such as trajectory in the tube, trajectory in water, vehicle attitude and inner load. The analysis indicates that the calculation results can catch the characteristic of underwater vehicle’s vertical sub-launching process, and the method is reasonable and feasible.
