From Control Requirements to PIL Test: Development of a Structure to Autopilot Implementation

This article presents the development of Autopilot (AP) blocks for a fixed-wing aircraft and the implementation of a Processor In the Loop (PIL) test platform. The AP entails the control, guidance, and navigation blocks. The control block design employed classical control theory considering a Piper...

Full description

Bibliographic Details
Main Authors: Marcelo H. Santos, Neusa M. F. Oliveira, Roberto D'Amore
Format: Article
Language:English
Published: IEEE 2021-01-01
Series:IEEE Access
Subjects:
Online Access:https://ieeexplore.ieee.org/document/9612203/
_version_ 1818835347656671232
author Marcelo H. Santos
Neusa M. F. Oliveira
Roberto D'Amore
author_facet Marcelo H. Santos
Neusa M. F. Oliveira
Roberto D'Amore
author_sort Marcelo H. Santos
collection DOAJ
description This article presents the development of Autopilot (AP) blocks for a fixed-wing aircraft and the implementation of a Processor In the Loop (PIL) test platform. The AP entails the control, guidance, and navigation blocks. The control block design employed classical control theory considering a Piper 4 aircraft model, and the MILF-8785C design requirements standard. The PIL test platform is composed of an AP running in a microcontroller and a simulated aircraft on a PC (Personal Computer). The results of three missions carried out on the PIL platform are presented. In these missions, the performed maneuvers are such that lateral and longitudinal controls are required. In all three cases, all predefined waypoints are achieved, indicating the success of the developed AP project. The AP test implemented in a microcontroller that can be embedded onto an aircraft for a real flight mission indicates the usefulness of the developed PIL platform.
first_indexed 2024-12-19T02:49:16Z
format Article
id doaj.art-7fb28224231d4c6fb5eb7ece57dcb9b5
institution Directory Open Access Journal
issn 2169-3536
language English
last_indexed 2024-12-19T02:49:16Z
publishDate 2021-01-01
publisher IEEE
record_format Article
series IEEE Access
spelling doaj.art-7fb28224231d4c6fb5eb7ece57dcb9b52022-12-21T20:38:45ZengIEEEIEEE Access2169-35362021-01-01915478815480310.1109/ACCESS.2021.31278469612203From Control Requirements to PIL Test: Development of a Structure to Autopilot ImplementationMarcelo H. Santos0Neusa M. F. Oliveira1https://orcid.org/0000-0003-2625-2161Roberto D'Amore2https://orcid.org/0000-0002-3456-0036IACIT, São José dos Campos, BrazilElectrical Engineering Department, ITA, São José dos Campos, BrazilElectrical Engineering Department, ITA, São José dos Campos, BrazilThis article presents the development of Autopilot (AP) blocks for a fixed-wing aircraft and the implementation of a Processor In the Loop (PIL) test platform. The AP entails the control, guidance, and navigation blocks. The control block design employed classical control theory considering a Piper 4 aircraft model, and the MILF-8785C design requirements standard. The PIL test platform is composed of an AP running in a microcontroller and a simulated aircraft on a PC (Personal Computer). The results of three missions carried out on the PIL platform are presented. In these missions, the performed maneuvers are such that lateral and longitudinal controls are required. In all three cases, all predefined waypoints are achieved, indicating the success of the developed AP project. The AP test implemented in a microcontroller that can be embedded onto an aircraft for a real flight mission indicates the usefulness of the developed PIL platform.https://ieeexplore.ieee.org/document/9612203/AutopilotPILRPAunmanned aerial systems
spellingShingle Marcelo H. Santos
Neusa M. F. Oliveira
Roberto D'Amore
From Control Requirements to PIL Test: Development of a Structure to Autopilot Implementation
IEEE Access
Autopilot
PIL
RPA
unmanned aerial systems
title From Control Requirements to PIL Test: Development of a Structure to Autopilot Implementation
title_full From Control Requirements to PIL Test: Development of a Structure to Autopilot Implementation
title_fullStr From Control Requirements to PIL Test: Development of a Structure to Autopilot Implementation
title_full_unstemmed From Control Requirements to PIL Test: Development of a Structure to Autopilot Implementation
title_short From Control Requirements to PIL Test: Development of a Structure to Autopilot Implementation
title_sort from control requirements to pil test development of a structure to autopilot implementation
topic Autopilot
PIL
RPA
unmanned aerial systems
url https://ieeexplore.ieee.org/document/9612203/
work_keys_str_mv AT marcelohsantos fromcontrolrequirementstopiltestdevelopmentofastructuretoautopilotimplementation
AT neusamfoliveira fromcontrolrequirementstopiltestdevelopmentofastructuretoautopilotimplementation
AT robertodamore fromcontrolrequirementstopiltestdevelopmentofastructuretoautopilotimplementation