Control of flight vehicles with the adjustable center of mass
Control of flight vehicles with the adjustable center of mass
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DOI:
10.3103/s1068799816030053
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发表时间:
--
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影响因子:
0.0
通讯作者:
V. A. Afanas’ev
中科院分区:
文献类型:
--
作者:
V. A. Afanas’ev; G. L. Degtyarev; V. I. Kiselev; A. S. Meshchanov
We resolve a problem how to control the longitudinal angular motion of flight vehicles (FV) having a system to displace the center of mass in the transverse direction. A structure is determined and a control law is established to start up and shutdown the engines. Formulas to determine the control parameters are obtained.