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Zuhri, Muhammad Rizki
Politeknik Negeri Bandung
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Flight Control Design for Rudder Failure Event on Cessna 172 Aircraft Zuhri, Muhammad Rizki
Indonesian Journal of Aerospace Vol. 23 No. 1 (2025): Indonesian Journal Of Aerospace
Publisher : BRIN Publishing

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.55981/ijoa.2025.9106

Abstract

The Cessna 172, a widely used small commercial aircraft, is renowned for its stabilityin both longitudinal and lateral-directional dimensions. Despite its intrinsic stability, arobust control system is essential to mitigate potential failures, such as rudder malfunctions.This study developed and simulated a control system for the Cessna 172 underrudder failure conditions, relying solely on aileron input for heading control. Using a linearstate-space approach implemented in Matlab/Simulink, the control system incorporatedyaw damping, roll damping, and heading hold for stability and waypoint tracking. Initialsimulations showed that the controller could guide the aircraft to the destination waypointbut exhibited significant deviations of up to 20% under constant rudder inputs. Controllermodification to the PID controller significantly improved performance, reducing deviationsto a maximum of only 0.1% for ±5° rudder input. These results demonstrate the effectivenessof the proposed control system in compensating for rudder failure, though slightoscillations observed at the start of the trajectory suggest the need for further refinement.This research underscores the potential for adaptive and unconventional control methodsto enhance safety and reliability in small aircraft operations.
Station-Keeping Simulation and Planning for LAPAN-A4 Satellite Using Finite-Burn Thruster Zuhri, Muhammad Rizki; Poetro, Ridanto Eko
Indonesian Journal of Aerospace Vol. 19 No. 1 (2021)
Publisher : BRIN Publishing

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.30536/j.jtd.2021.v19.a3474

Abstract

To be a Sun-synchronous orbit (SSO), the orbit must have a certain value of nodal precession rate, which equals to 360°/year. However, the value of nodal precession rate is usually drifted by orbit perturbations, mainly by the oblateness of the Earth and atmospheric drag, to be no longer 360°/year as expected for SSO. Thus, the local time of the satellite will change too, so it needs to be corrected by some correction maneuvers. In this research, the authors studied about station-keeping planning for SSO satellite via inclination correction maneuver by simulation using GMAT, a software developed by NASA, with a finite-burn propulsion approach. In this research, LAPAN-A4 satellite is chosen to be the satellite that will be simulated. Some alternative plans of inclination correction maneuver based on maneuvering periods are chosen, they are maneuver for every 2 months, 4 months, 6 months, 12 months, and 24 months. The simulation results show that the optimal station keeping planning is the maneuver for every 2 months. This alternative gives the lowest fuel consumption so that the fuel and launch cost will be minimum, and the local time drift that is still may be tolerated.
Mewujudkan Pemberdayaan Masyarakat Melalui Pelatihan Perawatan Pesawat Udara Khususnya Mesin Turbin Gas Bagi Guru-Guru SMKN 12 Bandung Lenny Iryani; Maria Fransisca Soetanto; Syarif Hidayat; Mochammad Luthfi; Budi Hartono; Radi Suradi Kartanegara; Teguh Wibowo; Yohanes Sinung Nugroho; Muhammad Rizki Zuhri; Citra Asti Rosalia; Zaim Sidqi Islami
AMMA : Jurnal Pengabdian Masyarakat Vol. 4 No. 5 : Juni (2025): AMMA : Jurnal Pengabdian Masyarakat
Publisher : CV. Multi Kreasi Media

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Abstract

This program is aimed for teachers from SMK N 12 Bandung. Through this PKM (Community Service Program), it is expected that the training participants will gain insights and enhanced knowledge regarding aircraft maintenance, particularly the maintenance of gas turbine engines. The training was conducted at the Propulsion Laboratory, Aeronautical Engineering Hangar, Department of Mechanical Engineering, from October 12 to 16, 2021. The aircraft engine maintenance training began with a pre-test to assess participants' initial knowledge of aircraft engine maintenance. At the end of the training, a post-test was conducted to measure the improvement in their understanding and knowledge. The outcome of this PKM activity is a certificate of participation in the aircraft maintenance training, specifically focused on gas turbine engines.
Co-Authors Ajeng Ayu Milanti Budi Hartono Budi Hartono Budi Hartono Citra Asti Rosalia Citra Asti Rosalia Citra Asti Rosalia Defrianto Pratama Destri Muliastri Devi Eka Septiyani Arifin Dewi, Yunita Citra Faturrohim, Luqman Fauzan, Nofrijal Hasanah, Rahmawati Indriyanto, Toto Lenny Iryani Mochammad Luthfi Muhammad Daffa Hauzaan Nofrijal Fauzan Poetro, Ridanto Eko Radi Suradi Kartanegara Rhamadhan, Firman Soetanto, Maria F Soetanto, Maria Fransisca Sri Widarti Syarif Hidayat Teguh Wibowoo Wibowo, Singgih Satrio Yohanes Sinung Nugroho Zaim Sidqi Islami Zaim Sidqi Islami Zainuddin Zainuddin