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Mathematical Problems in Engineering
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Mathematical Problems in Engineering
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2019
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Article
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Tab 1
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Research Article
Finite-Horizon Optimal Tracking Guidance for Aircraft Based on Approximate Dynamic Programming
Table 1
Simulation condition.
Parameters
Initial value
Final value
x (m)
0
80000
y (m)
12000
35000
0
0
m (kg)
150
80
V (m/s)
280
“
” means value range from minimum to maximum.