发明名称 |
Particle swarm-based micro air launch vehicle trajectory optimization method |
摘要 |
The particle swarm-based micro air launch vehicle trajectory optimization method is carried out by formulating a parameter optimization problem, which is solved using a particle swarm optimization procedure. The optimization problem is formulated using a single objective function having the explicit objective to maximize the payload mass. Constraints on terminal conditions are imposed. |
申请公布号 |
US8332085(B2) |
申请公布日期 |
2012.12.11 |
申请号 |
US20100871649 |
申请日期 |
2010.08.30 |
申请人 |
OMAR HANAFY M.;IDRES MOUMEN M.;KAFAFY RAED;KING FAHD UNIVERSITY OF PETROLEUM AND MINERALS |
发明人 |
OMAR HANAFY M.;IDRES MOUMEN M.;KAFAFY RAED |
分类号 |
B64G1/36 |
主分类号 |
B64G1/36 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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