Suboptimal Midcourse Guidance with Terminal-Angle Constraint for Hypersonic Target Interception
For the problem of hypersonic target interception, a novel midcourse guidance method with terminal-angle constraint is proposed. Referring to the air-breathing and the boost-gliding hypersonic targets, flight characteristics and difficulties of interception are analyzed, respectively. The requiremen...
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| Hauptverfasser: | , , , |
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| Format: | Artigo |
| Sprache: | Inglês |
| Veröffentlicht: |
Wiley
2019-01-01
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| Schriftenreihe: | International Journal of Aerospace Engineering |
| Online-Zugang: | http://dx.doi.org/10.1155/2019/6161032 |
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