Development Steps of Avionics and Flight Control System of Flight Vehicle
Abstract
The success of a research is highly dependent on the method adopted, especially research related to dangerous and expensive matters which will certainly require special handling in the development or maintenance steps. One of them is research related to space technology such as aviation and rocketry technology, which is very dependent on the design model of the flying vehicle and, in general, will always use simulation to ensure that the entire system being built is carried out safely and can be implemented properly according to plan. In the development of the prototype flying vehicle, especially the development of the avionics and flight control system, the vehicle will go through sequential simulation steps from Software in the Loop Simulation (SILS), Hardware in the Loop Simulation (HILS), and Ready-to-Fly System (RTFS). In this paper, the simulation steps will be described with the intention of facilitating integration and testing of each sub-system being developed, testing the control strategy applied or eliminating bugs if something goes wrong. In the end, with a series of flying vehicle simulations, it can be developed quickly and cost-effectively, including saving human resources.
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References
S. N. Kilo and P. H. Nyazungu, “Prevention and Management of Risks Related to Radiological and Nuclear Materials under International Nuclear Law: Case Study of the Democratic Republic of Congo,” Open J. Soc. Sci., vol. 9, no. 4, pp. 380–412, 2021, doi: https://doi.org/10.4236/jss.2021.94029.
W. Peng, Q. Zhang, T. Yang, and Z. Feng, “A high-precision dynamic model of a sounding rocket and rapid wind compensation method research,” Adv. Mech. Eng., vol. 9, no. 7, p. 1687814017713944, Jul. 2017, doi: 10.1177/1687814017713944.
M. Naderi, H. Karimi, and L. Guozhu, “Modeling the effect of reusability on the performance of an existing LPRE,” Acta Astronaut., vol. 181, pp. 201–216, 2021, doi: https://doi.org/10.1016/j.actaastro.2020.12.001.
P. Sai Teja, B. Sudhakar, A. D. Dhass, R. Krishna, and M. Sreenivasan, “Numerical and experimental analysis of hydroxyl-terminated poly-butadiene solid rocket motor by using ANSYS,” Mater. Today Proc., vol. 33, pp. 308–314, 2020, doi: https://doi.org/10.1016/j.matpr.2020.04.097.
P. Iguniwei, M. Y’au, and S. Okeniyi, “Apogee Measurement of a Polyvinyl Chloride Rocket Using a Sugar Composite Propellant and Open Source Computer Rocket Simulation Software,” Int. J. Sci. Eng. Appl., vol. 7, pp. 303–306, Sep. 2018, doi: 10.7753/IJSEA0709.1011.
H. Y. Irwanto, I. E. Putro, and Saeri, “HILS of FPV-2600 UAV using MyRIO-1950 as Optimal Flight Control System,” Int. J. Adv. Sci. Eng. Inf. Technol., vol. 11, no. 5, pp. 1780–1786, 2021, doi: http://dx.doi.org/10.18517/ijaseit.11.5.11919.
Y. Yun, J. Seo, K. Park, J. Huh, J. Lim, and S. Kwon, “Integration validation of key components for small sounding rockets,” Aerosp. Sci. Technol., vol. 100, p. 105823, 2020, doi: https://doi.org/10.1016/j.ast.2020.105823.
R. A. Duhri, “Guidance and control of 2nd stage RKX-200EB missile using proportional navigation approach,” 2020, doi: https://doi.org/10.1063/5.0060045.
B. I. Okoli, O. S. Sholiyi, and R. O. Durojaye, “Design, Analysis and Simulation of a Single Stage Rocket (Launch Vehicle) Using RockSim,” Int. J. Sci. Eng. Appl., vol. 10, no. 4, pp. 34–39, 2021, doi: 10.7753/IJSEA1004.1002.
F. M. Cantri, M. H. Bisri, and H. Y. Irwanto, “Realtime Simulation for Rocket Using Visual Programming,” in 2022 IEEE 8th Information Technology International Seminar (ITIS), 2022, pp. 150–155, doi: 10.1109/ITIS57155.2022.10010182.
H. Haqq, “Analysis Ballistic Flight and Design of Control System RKX200TJ/Booster at Rocket Booster and Climb Phases,” J. Teknol. Dirgant., vol. 18, no. 2, pp. 169–178, 2020, doi: http://dx.doi.org/10.30536/j.jtd.2020.v18.a3438.
A. Sabah Al-Araji, “Development of a Swing-Tracking Sliding Mode Controller Design for Nonlinear Inverted Pendulum System via Bees-Slice Genetic Algorithm,” Eng. Technol. J., vol. 34, no. 15, pp. 2897–2910, 2016, doi: 10.30684/etj.34.15A.11.
R. Sumathi and M. Usha, “Pitch and Yaw Attitude Control of a Rocket Engine Using Hybrid Fuzzy- PID Controller,” Open Autom. Control Syst. J., vol. 6, pp. 29–39, 2014.
H. Li, Y. Zhang, X. Liu, and J. Zhang, “Control System Design for Guided Rocket Base on Adaptive Sliding Mode Control,” in 2020 IEEE International Conference on Information Technology,Big Data and Artificial Intelligence (ICIBA), 2020, vol. 1, pp. 1462–1465, doi: 10.1109/ICIBA50161.2020.9276913.
Y. Shi, Y. Cheng, and Y. Gao, “A New Generation of Hardware-in-the-loop Simulation Technology Combined with High-performance Computers and Digital Twins,” J. Phys. Conf. Ser., vol. 2218, no. 1, p. 12032, 2022, doi: 10.1088/1742-6596/2218/1/012032.
P. Sarhadi and S. Yousefpour, “State of the art: hardware in the loop modeling and simulation with its applications in design, development and implementation of system and control software,” Int. J. Dyn. Control, vol. 3, Jan. 2014, doi: 10.1007/s40435-014-0108-3.
T. Li, A. M. Esteban, and S. Zhang, “Enhanced disturbance rejection control based test rocket control system design and validation,” ISA Trans., vol. 84, pp. 31–42, 2019, doi: https://doi.org/10.1016/j.isatra.2018.08.023.
X. Fan, X. Bai, Z. Jiang, L. Liu, and S. Zhang, “Design and Verification of Attitude Control System for a Boost-Glide Rocket,” IEEE Access, vol. 9, pp. 136360–136372, 2021, doi: 10.1109/ACCESS.2021.3117704.
Y. Gao, J. Wang, S. Gao, and J. Ding, “A General Integrated Design and Control Strategy Considering System Decomposition With Application to a Rocket Flight Attitude Control System,” IEEE/ASME Trans. Mechatronics, vol. 25, no. 6, pp. 2657–2666, 2020, doi: 10.1109/TMECH.2020.2987853.
H. Y. Irwanto, “Development of autonomous controller system of high speed UAV from simulation to ready to fly condition,” J. Phys. Conf. Ser., vol. 962, no. 1, p. 12015, 2018, doi: 10.1088/1742-6596/962/1/012015.
H. Y. Irwanto and E. Artono, “Correlation of Hardware in the Loop Simulation (HILS) and real control vehicle flight test for reducing flight failures,” J. Phys. Conf. Ser., vol. 1130, no. 1, p. 12014, 2018, doi: 10.1088/1742-6596/1130/1/012014.
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