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An S-type Ascent Trajectory Control Method Based on Scramjet Engine Working Boundary of RBCC
An S-type Ascent Trajectory Control Method Based on Scramjet Engine Working Boundary of RBCC
2021
Mingang Zhang
Jianhui Liu
Hui Liu
Liu Ming
Ming Yang
Xing Gao
Yinghui Gong
Mao-Tang
Jiajia Hou
Keywords:
trajectory control
Boundary (topology)
scramjet engine
Aerospace engineering
Computer science
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