Development Steps of Avionics and Flight Control System of Flight Vehicle

Development Steps of Avionics and Flight Control System of Flight Vehicle

software in the loop simulation (SILS); hardware in the loop simulation (HILS); ready to fly system (RTFS)

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 flying vehicle prototype, 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. And in the end, with a series of flying vehicle simulations, it can
be developed quickly, cost-effectively, including saving human resources

Herma Yudhi Irwanto, Purnomo Yusgiantoro, Zainal Abidin S., Romie O. Bura, Aris Sarjito , Oka Sudiana, Faisa Lailiyul M

http://jurnal.iaii.or.id

Professional Organization Ikatan Ahli Informatika Indonesia (IAII)/Indonesian Informatics Experts Association

August 2023

Sri Wahyuni

ISSN Media Electronic: 2580-0760

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