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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
/
2019
/
Article
/
Tab 2
/
Research Article
Suboptimal Midcourse Guidance with Terminal-Angle Constraint for Hypersonic Target Interception
Table 2
Convergence results of impact angle constrained guidance.
Default
60000
0
170
0.015
Real
59981
170.016
Default
60000
0
180
-0.051
Real
59959
179.958
Default
60000
0
190
-0.104
Real
59945
189.915