A Real-Time Linux system for autonomous navigation and flight attitude control of an uninhabited aerial vehicle

Author(s):  
C.E. Hall
Sensors ◽  
2021 ◽  
Vol 21 (7) ◽  
pp. 2534
Author(s):  
Oualid Doukhi ◽  
Deok-Jin Lee

Autonomous navigation and collision avoidance missions represent a significant challenge for robotics systems as they generally operate in dynamic environments that require a high level of autonomy and flexible decision-making capabilities. This challenge becomes more applicable in micro aerial vehicles (MAVs) due to their limited size and computational power. This paper presents a novel approach for enabling a micro aerial vehicle system equipped with a laser range finder to autonomously navigate among obstacles and achieve a user-specified goal location in a GPS-denied environment, without the need for mapping or path planning. The proposed system uses an actor–critic-based reinforcement learning technique to train the aerial robot in a Gazebo simulator to perform a point-goal navigation task by directly mapping the noisy MAV’s state and laser scan measurements to continuous motion control. The obtained policy can perform collision-free flight in the real world while being trained entirely on a 3D simulator. Intensive simulations and real-time experiments were conducted and compared with a nonlinear model predictive control technique to show the generalization capabilities to new unseen environments, and robustness against localization noise. The obtained results demonstrate our system’s effectiveness in flying safely and reaching the desired points by planning smooth forward linear velocity and heading rates.


2015 ◽  
Vol 74 (1) ◽  
Author(s):  
Muhammad Zaki Mustapa

This paper discusses on attitude control of a quadcopter unmanned aerial vehicle (UAV) in real time application. Newton-Euler equation is used to derive the model of system and the model characteristic is analyzed. The paper describes the controller design method for the hovering control of UAV automatic vertical take-off system. In order to take-off the quadcopter and stable the altitude, PID controller has been designed. The scope of study is to develop an altitude controller of the vertical take-off as realistic as possible. The quadcopter flight system has nonlinear characteristics. A simulation is conducted to test and analyze the control performance of the quadcopter model. The simulation was conducted by using Mat-lab Simulink. On the other hand, for the real time application, the PCI-1711 data acquisition card is used as an interface for controller design which routes from Simulink to hardware. This study showed the controller designs are implemented and tuned to the real system using Real Time Windows Target approach by Mat-Lab Simulink.


Energies ◽  
2021 ◽  
Vol 14 (10) ◽  
pp. 2810
Author(s):  
Krzysztof Naus ◽  
Piotr Szymak ◽  
Paweł Piskur ◽  
Maciej Niedziela ◽  
Aleksander Nowak

Undoubtedly, Low-Altitude Unmanned Aerial Vehicles (UAVs) are becoming more common in marine applications. Equipped with a Global Navigation Satellite System (GNSS) Real-Time Kinematic (RTK) receiver for highly accurate positioning, they perform camera and Light Detection and Ranging (LiDAR) measurements. Unfortunately, these measurements may still be subject to large errors-mainly due to the inaccuracy of measurement of the optical axis of the camera or LiDAR sensor. Usually, UAVs use a small and light Inertial Navigation System (INS) with an angle measurement error of up to 0.5∘ (RMSE). The methodology for spatial orientation angle correction presented in the article allows the reduction of this error even to the level of 0.01∘ (RMSE). It can be successfully used in coastal and port waters. To determine the corrections, only the Electronic Navigational Chart (ENC) and an image of the coastline are needed.


2021 ◽  
Vol 9 (4) ◽  
pp. 405
Author(s):  
Raphael Zaccone

While collisions and groundings still represent the most important source of accidents involving ships, autonomous vessels are a central topic in current research. When dealing with autonomous ships, collision avoidance and compliance with COLREG regulations are major vital points. However, most state-of-the-art literature focuses on offline path optimisation while neglecting many crucial aspects of dealing with real-time applications on vessels. In the framework of the proposed motion-planning, navigation and control architecture, this paper mainly focused on optimal path planning for marine vessels in the perspective of real-time applications. An RRT*-based optimal path-planning algorithm was proposed, and collision avoidance, compliance with COLREG regulations, path feasibility and optimality were discussed in detail. The proposed approach was then implemented and integrated with a guidance and control system. Tests on a high-fidelity simulation platform were carried out to assess the potential benefits brought to autonomous navigation. The tests featured real-time simulation, restricted and open-water navigation and dynamic scenarios with both moving and fixed obstacles.


2011 ◽  
Vol 130-134 ◽  
pp. 2684-2687 ◽  
Author(s):  
Kai Xu ◽  
Yan Lv ◽  
Guang Jin

Semi-physical simulation of attitude control system is the more synthetically test and verify for designing of small satellite control system. It is an important means of small satellite development. However, the results of current semi-physical simulation system have a lot of non-intuitive. Compare with the actual environment, the simulation environment still has striking disparity. So the shortcomings affect precision of simulation. Based on the virtual display technology, the group semi-physical simulation system has been constructed for attitude control of small satellite due to the combination with xPC real-time environment, the simulation computer, high-precision single-axis air-bearing turntable, reaction wheel, air thrust device, fiber gyroscopes, sensors synchronizer, power subsystem and wireless devices virtual display computer etc. Semi-physical simulation achieved the visual simulation in orbit and tracked new information of virtual environment of space into real-time simulation computer. Simulation results show that the simulation system for real-time attitude and orbit position of small satellite semi-physical simulation has an excellent display effect. At the same time, Real-time transfuse of orbit information provides a more accurate space environment simulation. The simulation system of small satellite attitude control to design and evaluate the more direct and convenient.


Sensors ◽  
2021 ◽  
Vol 21 (12) ◽  
pp. 3943
Author(s):  
Nicolas Montés ◽  
Francisco Chinesta ◽  
Marta C. Mora ◽  
Antonio Falcó ◽  
Lucia Hilario ◽  
...  

This paper presents a real-time global path planning method for mobile robots using harmonic functions, such as the Poisson equation, based on the Proper Generalized Decomposition (PGD) of these functions. The main property of the proposed technique is that the computational cost is negligible in real-time, even if the robot is disturbed or the goal is changed. The main idea of the method is the off-line generation, for a given environment, of the whole set of paths from any start and goal configurations of a mobile robot, namely the computational vademecum, derived from a harmonic potential field in order to use it on-line for decision-making purposes. Up until now, the resolution of the Laplace or Poisson equations has been based on traditional numerical techniques unfeasible for real-time calculation. This drawback has prevented the extensive use of harmonic functions in autonomous navigation, despite their powerful properties. The numerical technique that reverses this situation is the Proper Generalized Decomposition. To demonstrate and validate the properties of the PGD-vademecum in a potential-guided path planning framework, both real and simulated implementations have been developed. Simulated scenarios, such as an L-Shaped corridor and a benchmark bug trap, are used, and a real navigation of a LEGO®MINDSTORMS robot running in static environments with variable start and goal configurations is shown. This device has been selected due to its computational and memory-restricted capabilities, and it is a good example of how its properties could help the development of social robots.


2015 ◽  
Author(s):  
Χρήστος Παπαχρήστος

This Dissertation addresses the design and development of small-scale UnmannedAerial Vehicles of the TiltRotor class, alongside their autonomous navigation requirements,including the fully-onboard state estimation, high-efficiency flight control,and advanced environment perception.Starting with an educated Computer Assisted Design-based methodology, a mechanicallyrobust, customizable, and repeatable vehicle build is achieved, relyingon high-quality Commercially Available Off-The Shelf equipment –sensors, actuators,structural components–, optionally aided by Rapid Prototyping technology.A high-fidelity modeling process is conducted, incorporating the rigid-body dynamics,aerodynamics, and the actuation subsystem dynamics, exploiting fistprincipleapproaches, Frequency Domain System Identification, as well as computationaltools. Considering the most significant phenomena captured in thisprocess, a more simplified PieceWise Affine system model representation is developedfor control purposes –which however incorporates complexities such as flight(state) envelope-associated aerodynamics, the differentiated effects of the directthrust-vectoring (rotor-tilting) and the underactuated (body-pitching) actuationauthorities, as well as their interferences through rigid-body coupling–.Despite the switching system dynamics, and –as thoroughly elaborated– theirreliance on constrained manipulated variables, to maintain a meaningful controlorientedrepresentation, the real-time optimal flight control of the TiltRotor vehicleis achieved relying on a Receding Horizon methodology, and more specifically anexplicit Model Predictive Control framework. This synthesis guarantees globalstability of the switching dynamics, observance of state and control input constraints,response optimality, as well as efficient execution on low computationa power modules due to its explicit representation. Accompanied by a proper Lowand-Mid-LevelControl synthesis, this scheme provides exceptional flight handlingqualities to the aerial vehicle, particularly in the areas of aggressive maneuveringand high-accuracy trajectory tracking.Moreover, the utility of TiltRotor vehicles in the field of aerial robotic forcefulphysical interaction is researched. Exploiting the previously noted properties ofthe PieceWise Affine systems Model Predictive Control strategy, the guaranteedstabilityFree-Flight to Physical-Interaction switching of the system is achieved,effectively bringing the aerial vehicle into safe, controlled physical contact withthe surface of structures in the environment.More importantly, employing rotor-tilting actuation –collectively and differentially–significant forces and moments can be applied onto the environment, while via thestandard underactuated authority the vehicle maintains a stable hovering-attitudepose, where the system’s disturbance rejection properties are maximized. Overall,the complete control framework enables coming into physical contact with environmentstructures, and manipulating the enacted forces and moments. Exploitingsuch capabilities the TiltRotor is used to achieve the execution of physicallydemandingwork-tasks (surface-grinding) and the manipulation of realisticallysizedobjects (of twice its own mass) via pushing.Additionally, the fully-onboard state estimation problem is tackled by implementingdata fusion of measurements derived from inertial sensors and customdevelopedcomputer vision algorithms which employ Homography and OpticalFlow calculation. With a proper sensorial setup, high-rate and robust ego-motionestimation is achieved, enabling the controlled aggressive maneuverability withoutreliance on external equipment, such as motion capture systems or GlobalPositioning System coverage.Finally, a hardware/software framework is developed which adds advanced autonomousperception and navigation capabilities to small-scale unmanned vehicles,employing stereo vision and integrating state-of-the art solutions for incrementalenvironment building, dense reconstruction and mapping, and point-to-pointcollision-free navigation. Within this framework, algorithms which enable the detection,segmentation, (re-)localization, and mobile tracking –and avoidance– of adynamic subject within the aerial vehicle’s operating space are developed, substantiallyincreasing the operational potential of autonomous aircraft within dynamicenvironments and/or dynamically evolving missions.


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