Legendre Pseudo-Spectral Method for Missile Trajectory Optimization with Free Final Time
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-19-2635-8_42
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5. Yogaswara Y, Hong S-M, Tahk M-J, Shin H-S (2017) Impact angle control guidance synthesis for evasive maneuver against intercept missile. Int J Aeronaut Space Sci 18(4):719–728
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