TY - GEN
T1 - Testing of an infrared-based SACLOS guidance in a subsonic wind tunnel
AU - Nugroho, Larasmoyo
AU - Al-Fadli, M. Hanifuddin
AU - Andiarti, Rika
AU - Wijaya, Sastra Kusuma
N1 - Funding Information:
This work as part of the author’s dissertation research is supported by LAPAN PUSTEKROKET. The high acknowledgment must be given to its Director, Mr. Sutrisno, and Vices, Mrs. Lilis Mariani and Mr. Heru Supriyatno.
Publisher Copyright:
© 2021 Author(s).
PY - 2021/9/13
Y1 - 2021/9/13
N2 - Anti-tank guided missiles generally have short to medium travel range, therefore it is suitable to use CLOS (command line-of-sight) as a way to guide them, due to its cost-efficient architecture configuration. To design, develop, and validate this SACLOS (semi-automatic command line of sight) guidance technology, a Hardware-in-the-Loop (HWIL) simulation, and function testing was conducted in an open subsonic wind tunnel environment. The algorithm and hardware architecture are to be tested non-destructively steering the missile against a 20 m/s air velocity. The mission is to follow the rule-based SACLOS desired command exerted to the missile, and the experiments confirm this accomplishment.
AB - Anti-tank guided missiles generally have short to medium travel range, therefore it is suitable to use CLOS (command line-of-sight) as a way to guide them, due to its cost-efficient architecture configuration. To design, develop, and validate this SACLOS (semi-automatic command line of sight) guidance technology, a Hardware-in-the-Loop (HWIL) simulation, and function testing was conducted in an open subsonic wind tunnel environment. The algorithm and hardware architecture are to be tested non-destructively steering the missile against a 20 m/s air velocity. The mission is to follow the rule-based SACLOS desired command exerted to the missile, and the experiments confirm this accomplishment.
UR - http://www.scopus.com/inward/record.url?scp=85115339194&partnerID=8YFLogxK
U2 - 10.1063/5.0060368
DO - 10.1063/5.0060368
M3 - Conference contribution
AN - SCOPUS:85115339194
T3 - AIP Conference Proceedings
BT - 8th International Seminar on Aerospace Science and Technology, ISAST 2020
A2 - Kurniawan, Farohaji
A2 - Kurniawati, Frida
A2 - Bahri, Sayr
A2 - Santosa, Cahya Edi
A2 - Hasbi, Wahyudi
A2 - Septanto, Harry
A2 - Hermawan, Eddy
PB - American Institute of Physics Inc.
T2 - 8th International Seminar on Aerospace Science and Technology, ISAST 2020
Y2 - 17 November 2020
ER -