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Kinetik: Game Technology, Information System, Computer Network, Computing, Electronics, and Control
Published by Universitas Muhammadiyah Malang
ISSN : 25032259     EISSN : 25032267     DOI : -
Core Subject : Science, Engineering,
Computer Science & IT Control & Systems Engineering Electrical & Electronics Engineering Energy Engineering
Kinetik: Game Technology, Information System, Computer Network, Computing, Electronics, and Control was published by Universitas Muhammadiyah Malang. journal is open access journal in the field of Informatics and Electrical Engineering. This journal is available for researchers who want to improve their knowledge in those particular areas and intended to spread the knowledge as the result of studies. KINETIK journal is a scientific research journal for Informatics and Electrical Engineering. It is open for anyone who desire to develop knowledge based on qualified research in any field. Submitted papers are evaluated by anonymous referees by double-blind peer review for contribution, originality, relevance, and presentation. The Editor shall inform you of the results of the review as soon as possible, hopefully within 4 - 8 weeks. The research article submitted to this online journal will be peer-reviewed at least 2 (two) reviewers. The accepted research articles will be available online following the journal peer-reviewing process.
Arjuna Subject : -
Articles 22 Documents
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Search results for , issue "Vol 2, No 4, November-2017" : 22 Documents clear
Improving MoWaS Application Backbone System for The Effectiveness of Responsive Behaviour in Facing Crime Threats and Emergency Situations Arif Arizal; Syariful Alim
Kinetik: Game Technology, Information System, Computer Network, Computing, Electronics, and Control Vol 2, No 4, November-2017
Publisher : Universitas Muhammadiyah Malang

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.22219/kinetik.v2i4.250

Abstract

MoWaS is a mobile-based supporting application aiming to improve the rapid response against crime crime and emergency situations. The evaluation of MoWaS version 1.0 has 3 flaws. First, it is unable to create a group. Second, the MoWaS version 1.0 application is able to detect the current location of the alert sender but there is no feature to display information about nearby MoWaS application users. Third, MoWaS application version 1.0 is also not integrated with the official service or government agency related to the types of occurring crime. The results of the design revision and analysis were made including the MoWaS system architecture design, the MoWaS system flow described in the form of flowchart, and the MoWaS system interface design. The results of the analysis and design of MoWaS backbone system can be used as the basis for improvement of MoWaS system development. Hence, it can be concluded that the MoWaS application version 2.0 has a better work system than the previous version.
Aircraft Pitch Control Design using Observer-State Feedback Control Hanum Arrosida; Mohammad Erik Echsony
Kinetik: Game Technology, Information System, Computer Network, Computing, Electronics, and Control Vol 2, No 4, November-2017
Publisher : Universitas Muhammadiyah Malang

Show Abstract | Download Original | Original Source | Check in Google Scholar | Full PDF (386.706 KB) | DOI: 10.22219/kinetik.v2i4.267

Abstract

Pitch is a movement of an aircraft achieved by tilting the elevator control which makes the nose of aircraft ascend or descend. This research will design a control system that controls the slope of the x-axis or pitch with the observer-state feedback to keep the aircraft always in the position setpoint, the stabilization of the pitch angle at the value of 0 radians. The applied controller is tested under three different conditions based on the variation of the gain value of Q and R that will affect the observed gain matrix (L gain) and the matrix state-feedback gain (K gain). The variation with the gain value of Q = 10 and R = 0.1 is the best result of the three kinds of testing performed with the fastest stabilization processing time, that is 7 seconds, to reach a steady state condition and the minimum pitch angle deviation value is 0.08 radians. The use of the observer has a significant influence on the pitch angle deviation of the aircraft. When using the observer, the pitch angle deviation value is 0.08 radians, and 0.2 radians without the observer. The larger result of pitch deviation angle will affect the stability of the aircraft's motion and cause the slope of the movement on the x-axis become greater so that the aircraft is prone to fall.

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