AK, R. E., Prasetyo, M. R., & Hidayat, Z. (2018). Designing an Optimal Control LQT for Controlling and Guidance of Missile. Institut Teknologi Sepuluh Nopember.
Chicago Style (17th ed.) CitationAK, Rusdhianto Effendie, Muhamad Rafif Prasetyo, and Zulkifli Hidayat. Designing an Optimal Control LQT for Controlling and Guidance of Missile. Institut Teknologi Sepuluh Nopember, 2018.
MLA (8th ed.) CitationAK, Rusdhianto Effendie, et al. Designing an Optimal Control LQT for Controlling and Guidance of Missile. Institut Teknologi Sepuluh Nopember, 2018.
Warning: These citations may not always be 100% accurate.