Cost-Effective HWIL testing methodology for SALS guided missiles
Само за регистроване кориснике
2022
Конференцијски прилог (Објављена верзија)
Метаподаци
Приказ свих података о документуАпстракт
Verifying a new missile design requires a series of successful real-life tests on a firing range in various scenarios. Such an approach is extremely expensive and requires complex infrastructure and logistics. The costs of developing a new missile design can be significantly reduced by applying extensive and well thought out laboratory testing prior to any real-life test. Laboratory tests such as Hardware-In-The-Loop (HWIL) simulation enable the missile to be tested in a controlled environment inside a laboratory. HWIL testing methodology enables engineers to test the missile or its components in various simulated scenarios that correspond to real-life flights. Usually, a five-axis motion platform is used to perform HWIL simulation of terminal guidance. Three inner axes of the five-axis motion platform are used for simulation of the missiles body angles, while the two outer axes are used for simulation of the target movement relative to the missile. Such an approach requires spacious l...aboratories and expensive equipment. In this paper, we present a cost-effective HWIL testing methodology for Semi-Active-Laser-Seeker (SALS) guided missiles. The presented methodology requires only a three-axis motion platform and a fixed laser source. In the paper, we propose a two-stage HWIL testing procedure. In the first stage, the INS algorithm, guidance algorithm and autopilot algorithms are verified. In the second stage of the proposed HWIL testing methodology, the terminal guidance algorithm based on SALS angles is verified. Besides the HWIL testing methodology, we present the guidance law used in the testing procedure as well as the design of intercommunication between all the devices required to perform the tests. Next, the obtained results after each stage of the proposed HWIL testing methodology are presented and analyzed. Finally, a conclusion is drawn and limitations of the proposed testing methodology are explained.
Кључне речи:
Semi-Active Laser Seeker / Real-time computing / Missile guidance and control / Hardware in the loop / Embedded systems / 6DOF simulationИзвор:
Materials Today-Proceedings, 2022, 62, 2509-2515Издавач:
- Elsevier, Amsterdam
Финансирање / пројекти:
- company EDe-Pro - Engine Design and Production in Belgrade
DOI: 10.1016/j.matpr.2022.03.108
ISSN: 2214-7853
WoS: 000818797700023
Scopus: 2-s2.0-85127898081
Колекције
Институција/група
Mašinski fakultetTY - CONF AU - Todić, Ivana AU - Kuzmanović, Vladimir PY - 2022 UR - https://machinery.mas.bg.ac.rs/handle/123456789/3753 AB - Verifying a new missile design requires a series of successful real-life tests on a firing range in various scenarios. Such an approach is extremely expensive and requires complex infrastructure and logistics. The costs of developing a new missile design can be significantly reduced by applying extensive and well thought out laboratory testing prior to any real-life test. Laboratory tests such as Hardware-In-The-Loop (HWIL) simulation enable the missile to be tested in a controlled environment inside a laboratory. HWIL testing methodology enables engineers to test the missile or its components in various simulated scenarios that correspond to real-life flights. Usually, a five-axis motion platform is used to perform HWIL simulation of terminal guidance. Three inner axes of the five-axis motion platform are used for simulation of the missiles body angles, while the two outer axes are used for simulation of the target movement relative to the missile. Such an approach requires spacious laboratories and expensive equipment. In this paper, we present a cost-effective HWIL testing methodology for Semi-Active-Laser-Seeker (SALS) guided missiles. The presented methodology requires only a three-axis motion platform and a fixed laser source. In the paper, we propose a two-stage HWIL testing procedure. In the first stage, the INS algorithm, guidance algorithm and autopilot algorithms are verified. In the second stage of the proposed HWIL testing methodology, the terminal guidance algorithm based on SALS angles is verified. Besides the HWIL testing methodology, we present the guidance law used in the testing procedure as well as the design of intercommunication between all the devices required to perform the tests. Next, the obtained results after each stage of the proposed HWIL testing methodology are presented and analyzed. Finally, a conclusion is drawn and limitations of the proposed testing methodology are explained. PB - Elsevier, Amsterdam C3 - Materials Today-Proceedings T1 - Cost-Effective HWIL testing methodology for SALS guided missiles EP - 2515 SP - 2509 VL - 62 DO - 10.1016/j.matpr.2022.03.108 ER -
@conference{ author = "Todić, Ivana and Kuzmanović, Vladimir", year = "2022", abstract = "Verifying a new missile design requires a series of successful real-life tests on a firing range in various scenarios. Such an approach is extremely expensive and requires complex infrastructure and logistics. The costs of developing a new missile design can be significantly reduced by applying extensive and well thought out laboratory testing prior to any real-life test. Laboratory tests such as Hardware-In-The-Loop (HWIL) simulation enable the missile to be tested in a controlled environment inside a laboratory. HWIL testing methodology enables engineers to test the missile or its components in various simulated scenarios that correspond to real-life flights. Usually, a five-axis motion platform is used to perform HWIL simulation of terminal guidance. Three inner axes of the five-axis motion platform are used for simulation of the missiles body angles, while the two outer axes are used for simulation of the target movement relative to the missile. Such an approach requires spacious laboratories and expensive equipment. In this paper, we present a cost-effective HWIL testing methodology for Semi-Active-Laser-Seeker (SALS) guided missiles. The presented methodology requires only a three-axis motion platform and a fixed laser source. In the paper, we propose a two-stage HWIL testing procedure. In the first stage, the INS algorithm, guidance algorithm and autopilot algorithms are verified. In the second stage of the proposed HWIL testing methodology, the terminal guidance algorithm based on SALS angles is verified. Besides the HWIL testing methodology, we present the guidance law used in the testing procedure as well as the design of intercommunication between all the devices required to perform the tests. Next, the obtained results after each stage of the proposed HWIL testing methodology are presented and analyzed. Finally, a conclusion is drawn and limitations of the proposed testing methodology are explained.", publisher = "Elsevier, Amsterdam", journal = "Materials Today-Proceedings", title = "Cost-Effective HWIL testing methodology for SALS guided missiles", pages = "2515-2509", volume = "62", doi = "10.1016/j.matpr.2022.03.108" }
Todić, I.,& Kuzmanović, V.. (2022). Cost-Effective HWIL testing methodology for SALS guided missiles. in Materials Today-Proceedings Elsevier, Amsterdam., 62, 2509-2515. https://doi.org/10.1016/j.matpr.2022.03.108
Todić I, Kuzmanović V. Cost-Effective HWIL testing methodology for SALS guided missiles. in Materials Today-Proceedings. 2022;62:2509-2515. doi:10.1016/j.matpr.2022.03.108 .
Todić, Ivana, Kuzmanović, Vladimir, "Cost-Effective HWIL testing methodology for SALS guided missiles" in Materials Today-Proceedings, 62 (2022):2509-2515, https://doi.org/10.1016/j.matpr.2022.03.108 . .