Open AccessAltitude Control Design of LSU-05 Aircraft Using Abstraction Method
Author(s) -
Muhammad Afif Nasrul Anam,
Dieky Adzkiya,
Tahiyatul Asfihani
Publication year - 2019
Publication title -
journal of physics. conference series
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.21
H-Index - 85
eISSN - 1742-6596
pISSN - 1742-6588
DOI - 10.1088/1742-6596/1218/1/012027
Subject(s) - autopilot , abstraction , fixed wing , computer science , range (aeronautics) , control (management) , control logic , software , control engineering , control system , altitude (triangle) , systems engineering , engineering , wing , aerospace engineering , programming language , mathematics , artificial intelligence , geometry , philosophy , electrical engineering , epistemology
LAPAN Surveilance-05 (LSU-05) is a fixed wing type aircraft developed by LAPAN. This aircraft can be used for monitoring and mapping a very wide range of areas. In carrying out operational missions, the aircraft requires reliable control of autopilot to control flying altitudes, thus facilitating and able to support the mission and for aircraft safety. In the design of the control, we apply the abstraction method using software Pessoa. The design of the control with abstraction aims to design the control such that the closed loop system behavior satisfies the specifications in the form of simple temporal logic. In the experiments, we conduct two scenarios. For each scenario, we use different specification and different abstraction parameter.