Autonomous aircraft

Source: Wikipedia, the free encyclopedia.

An autonomous aircraft is an aircraft which flies under the control of automatic systems and needs no intervention from a human pilot. Most autonomous aircraft are unmanned aerial vehicle or drones. However, autonomous control systems are reaching a point where several air taxis and associated regulatory regimes are being developed.

History

Unmanned aerial vehicles

Winston Churchill and others waiting to watch the launch of a de Havilland Queen Bee target drone, 6 June 1941

The earliest recorded use of an unmanned aerial vehicle for warfighting occurred in July 1849,[1] serving as a balloon carrier (the precursor to the aircraft carrier)[2] Significant development of radio-controlled drones started in the early 1900s, and originally focused on providing practice targets for training military personnel. The earliest attempt at a powered UAV was A. M. Low's "Aerial Target" in 1916.[3]

Autonomous features such as the autopilot and automated navigation were developed progressively through the twentieth century, although techniques such as terrain contour matching (TERCOM) were applied mainly to cruise missiles.

Some modern drones have a high degree of autonomy, although they are not fully capable and the regulatory environment prohibits their widespread use in civil aviation. However some limited trials have been undertaken.

Passengers

As flight, navigation and communications systems have become more sophisticated, safely carrying passengers has emerged as a practical possibility. Autopilot systems are relieving the human pilot of progressively more duties, but the pilot currently remains necessary.

A number of air taxis are under development and larger autonomous transports are also being planned. The personal air vehicle is another class where from one to four passengers are not expected to be able to pilot the aircraft and autonomy is seen as necessary for widespread adoption.

Control system architecture

The computing capability of aircraft flight and navigation systems followed the advances of computing technology, beginning with analog controls and evolving into microcontrollers, then system-on-a-chip (SOC) and single-board computers (SBC).

Sensors

Position and movement sensors give information about the aircraft state. Exteroceptive sensors deal with external information like distance measurements, while exproprioceptive ones correlate internal and external states.[4]

Non-cooperative sensors are able to detect targets autonomously so they are used for separation assurance and collision avoidance.[5]

Degrees of freedom (DOF) refers to both the amount and quality of sensors on board: 6 DOF implies 3-axis gyroscopes and accelerometers (a typical inertial measurement unit – IMU), 9 DOF refers to an IMU plus a compass, 10 DOF adds a barometer and 11 DOF usually adds a GPS receiver.[6]

Actuators

UAV actuators include digital electronic speed controllers (which control the RPM of the motors) linked to motors/engines and propellers, servomotors (for planes and helicopters mostly), weapons, payload actuators, LEDs and speakers.

Software

UAV software called the flight stack or autopilot. The purpose of the flight stack is to obtain data from sensors, control motors to ensure UAV stability, and facilitate ground control and mission planning communication.[7]

UAVs are real-time systems that require rapid response to changing sensor data. As a result, UAVs rely on single-board computers for their computational needs. Examples of such single-board computers include Raspberry Pis, Beagleboards, etc. shielded with NavIO, PXFMini, etc. or designed from scratch such as NuttX, preemptive-RT Linux, Xenomai, Orocos-Robot Operating System or DDS-ROS 2.0.

Flight stack overview
Layer Requirement Operations Example
Firmware Time-critical From machine code to processor execution, memory access ArduCopter-v1, PX4
Middleware Time-critical Flight control, navigation, radio management PX4, Cleanflight, ArduPilot
Operating system Computer-intensive Optical flow, obstacle avoidance, SLAM, decision-making ROS, Nuttx, Linux distributions, Microsoft IOT

Civil-use open-source stacks include:

Due to the open-source nature of UAV software, they can be customized to fit specific applications. For example, researchers from the Technical University of Košice have replaced the default control algorithm of the PX4 autopilot.[8] This flexibility and collaborative effort has led to a large number of different open-source stacks, some of which are forked from others, such as CleanFlight, which is forked from BaseFlight and from which three other stacks are forked from.

Loop principles

Typical flight-control loops for a multirotor

UAVs employ open-loop, closed-loop or hybrid control architectures.

  • Open loop – This type provides a positive control signal (faster, slower, left, right, up, down) without incorporating feedback from sensor data.
  • Closed loop – This type incorporates sensor feedback to adjust behavior (reduce speed to reflect tailwind, move to altitude 300 feet). The PID controller is common. Sometimes, feedforward is employed, transferring the need to close the loop further.[9]

Communications

Most UAVs use a radio for remote control and exchange of video and other data. Early UAVs had only narrowband uplink. Downlinks came later. These bi-directional narrowband radio links carried command and control (C&C) and telemetry data about the status of aircraft systems to the remote operator. For very long range flights, military UAVs also use satellite receivers as part of satellite navigation systems. In cases when video transmission was required, the UAVs will implement a separate analog video radio link.

In most modern autonomous applications, video transmission is required. A broadband link is used to carry all types of data on a single radio link. These broadband links can leverage quality of service techniques to optimize the C&C traffic for low latency. Usually, these broadband links carry TCP/IP traffic that can be routed over the Internet.

Communications can be established with:

  • Ground control – a military ground control station (GCS). The MAVLink protocol is increasingly becoming popular to carry command and control data between the ground control and the vehicle.
  • Remote network system, such as satellite duplex data links for some military powers.[10] Downstream digital video over mobile networks has also entered consumer markets,[11] while direct UAV control uplink over the cellular mesh and LTE have been demonstrated and are in trials.[12]
  • Another aircraft, serving as a relay or mobile control station – military manned-unmanned teaming (MUM-T).[13]

As mobile networks have increased in performance and reliability over the years, drones have begun to use mobile networks for communication. Mobile networks can be used for drone tracking, remote piloting, over the air updates,[14] and cloud computing.[15]

Modern networking standards have explicitly considered autonomous aircraft and therefore include optimizations. The 5G standard has mandated reduced user plane latency to 1ms while using ultra-reliable and low-latency communications.[16]

Autonomy

Autonomous control basics

Basic autonomy comes from proprioceptive sensors. Advanced autonomy calls for situational awareness, knowledge about the environment surrounding the aircraft from exteroceptive sensors: sensor fusion integrates information from multiple sensors.[4]

Basic principles

One way to achieve autonomous control employs multiple control-loop layers, as in hierarchical control systems. As of 2016 the low-layer loops (i.e. for flight control) tick as fast as 32,000 times per second, while higher-level loops may cycle once per second. The principle is to decompose the aircraft's behavior into manageable "chunks", or states, with known transitions. Hierarchical control system types range from simple scripts to finite state machines, behavior trees and hierarchical task planners. The most common control mechanism used in these layers is the PID controller which can be used to achieve hover for a quadcopter by using data from the IMU to calculate precise inputs for the electronic speed controllers and motors.[citation needed]

Examples of mid-layer algorithms:

  • Path planning: determining an optimal path for vehicle to follow while meeting mission objectives and constraints, such as obstacles or fuel requirements
  • Trajectory generation (motion planning): determining control maneuvers to take in order to follow a given path or to go from one location to another[17][18]
  • Trajectory regulation: constraining a vehicle within some tolerance to a trajectory

Evolved UAV hierarchical task planners use methods like state tree searches or genetic algorithms.[19]

Autonomy features

UAV's degrees of autonomy

UAV manufacturers often build in specific autonomous operations, such as:

  • Self-level: attitude stabilization on the pitch and roll axes.
  • Altitude hold: The aircraft maintains its altitude using barometric pressure and/or GPS data.
  • Hover/position hold: Keep level pitch and roll, stable yaw heading and altitude while maintaining position using GNSS or inertial sensors.
  • Headless mode: Pitch control relative to the position of the pilot rather than relative to the vehicle's axes.
  • Care-free: automatic roll and yaw control while moving horizontally
  • Take-off and landing (using a variety of aircraft or ground-based sensors and systems; see also:Autoland)
  • Failsafe: automatic landing or return-to-home upon loss of control signal
  • Return-to-home: Fly back to the point of takeoff (often gaining altitude first to avoid possible intervening obstructions such as trees or buildings).
  • Follow-me: Maintain relative position to a moving pilot or other object using GNSS, image recognition or homing beacon.
  • GPS waypoint navigation: Using GNSS to navigate to an intermediate location on a travel path.
  • Orbit around an object: Similar to Follow-me but continuously circle a target.
  • Pre-programmed aerobatics (such as rolls and loops).

Functions

Full autonomy is available for specific tasks, such as airborne refueling[20] or ground-based battery switching; but higher-level tasks call for greater computing, sensing and actuating capabilities. One approach to quantifying autonomous capabilities is based on OODA terminology, as suggested by a 2002 US Air Force Research Laboratory, and used in the table below:[21]

United States Autonomous control levels chart
Level Level descriptor Observe Orient Decide Act
Perception/Situational awareness Analysis/Coordination Decision making Capability
10 Fully Autonomous Cognizant of all within battlespace Coordinates as necessary Capable of total independence Requires little guidance to do job
9 Battlespace Swarm Cognizance Battlespace inference – Intent of self and others (allied and foes).

Complex/Intense environment – on-board tracking

Strategic group goals assigned

Enemy strategy inferred

Distributed tactical group planning

Individual determination of tactical goal

Individual task planning/execution

Choose tactical targets

Group accomplishment of strategic goal with no supervisory assistance
8 Battlespace Cognizance Proximity inference – Intent of self and others (allied and foes)

Reduces dependence upon off-board data

Strategic group goals assigned

Enemy tactics inferred

ATR

Coordinated tactical group planning

Individual task planning/execution

Choose target of opportunity

Group accomplishment of strategic goal with minimal supervisory assistance

(example: go SCUD hunting)

7 Battlespace Knowledge Short track awareness – History and predictive battlespace

Data in limited range, timeframe and numbers

Limited inference supplemented by off-board data

Tactical group goals assigned

Enemy trajectory estimated

Individual task planning/execution to meet goals Group accomplishment of tactical goals with minimal supervisory assistance
6 Real Time

Multi-Vehicle Cooperation

Ranged awareness – on-board sensing for long range,

supplemented by off-board data

Tactical group goals assigned

Enemy trajectory sensed/estimated

Coordinated trajectory planning and execution to meet goals – group optimization Group accomplishment of tactical goals with minimal supervisory assistance

Possible: close air space separation (+/-100yds) for AAR, formation in non-threat conditions

5 Real Time

Multi-Vehicle Coordination

Sensed awareness – Local sensors to detect others,

Fused with off-board data

Tactical group plan assigned

RT Health Diagnosis Ability to compensate for most failures and flight conditions;

Ability to predict onset of failures (e.g. Prognostic Health Mgmt)

Group diagnosis and resource management

On-board trajectory replanning – optimizes for current and predictive conditions

Collision avoidance

Self accomplishment of tactical plan as externally assigned

Medium vehicle airspace separation (hundreds of yds)

4 Fault/Event Adaptative

Vehicle

Deliberate awareness – allies communicate data Tactical group plan assigned

Assigned Rules of Engagement

RT Health Diagnosis; Ability to compensate for most failures and flight conditions – inner loop changes reflected in outer loop performance

On-board trajectory replanning – event driven

Self resource management

Deconfliction

Self accomplishment of tactical plan as externally assigned

Medium vehicle airspace separation (hundreds of yds)

3 Robust Response to Real Time Faults/Events Health/status history & models Tactical group plan assigned

RT Health Diagnosis (What is the extent of the problems?)

Ability to compensate for most failures and flight conditions (i.e. adaptative inner loop control)

Evaluate status vs required mission capabilities

Abort/RTB is insufficient

Self accomplishment of tactical plan as externally assigned
2 Changeable mission Health/status sensors RT Health diagnosis (Do I have problems?)

Off-board replan (as required)

Execute preprogrammed or uploaded plans

in response to mission and health conditions

Self accomplishment of tactical plan as externally assigned
1 Execute Preplanned

Mission

Preloaded mission data

Flight Control and Navigation Sensing

Pre/Post flight BIT

Report status

Preprogrammed mission and abort plans Wide airspace separation requirements (miles)
0 Remotely

Piloted

Vehicle

Flight Control (attitude, rates) sensing

Nose camera

Telemetered data

Remote pilot commands

N/A Control by remote pilot

Medium levels of autonomy, such as reactive autonomy and high levels using cognitive autonomy, have already been achieved to some extent and are very active research fields.

Reactive autonomy

Reactive autonomy, such as collective flight, real-time collision avoidance, wall following and corridor centring, relies on telecommunication and situational awareness provided by range sensors: optic flow,[22] lidars (light radars), radars, sonars.

Most range sensors analyze electromagnetic radiation, reflected off the environment and coming to the sensor. The cameras (for visual flow) act as simple receivers. Lidars, radars and sonars (with sound mechanical waves) emit and receive waves, measuring the round-trip transit time. UAV cameras do not require emitting power, reducing total consumption.

Radars and sonars are mostly used for military applications.

Reactive autonomy has in some forms already reached consumer markets: it may be widely available in less than a decade.[4]

Cutting-edge (2013) autonomous levels for existing systems

Simultaneous localization and mapping

SLAM combines odometry and external data to represent the world and the position of the UAV in it in three dimensions. High-altitude outdoor navigation does not require large vertical fields-of-view and can rely on GPS coordinates (which makes it simple mapping rather than SLAM).[23]

Two related research fields are photogrammetry and LIDAR, especially in low-altitude and indoor 3D environments.

Swarming

Robot swarming refers to networks of agents able to dynamically reconfigure as elements leave or enter the network. They provide greater flexibility than multi-agent cooperation. Swarming may open the path to data fusion. Some bio-inspired flight swarms use steering behaviors and flocking.[clarification needed]

Future military potential

In the military sector, American Predators and Reapers are made for counterterrorism operations and in war zones in which the enemy lacks sufficient firepower to shoot them down. They are not designed to withstand antiaircraft defenses or air-to-air combat. In September 2013, the chief of the US Air Combat Command stated that current UAVs were "useless in a contested environment" unless crewed aircraft were there to protect them. A 2012 Congressional Research Service (CRS) report speculated that in the future, UAVs may be able to perform tasks beyond intelligence, surveillance, reconnaissance and strikes; the CRS report listed air-to-air combat ("a more difficult future task") as possible future undertakings. The Department of Defense's Unmanned Systems Integrated Roadmap FY2013-2038 foresees a more important place for UAVs in combat. Issues include extended capabilities, human-UAV interaction, managing increased information flux, increased autonomy and developing UAV-specific munitions. DARPA's project of systems of systems,[30] or General Atomics work may augur future warfare scenarios, the latter disclosing Avenger swarms equipped with High Energy Liquid Laser Area Defense System (HELLADS).[31]

Cognitive radio

Cognitive radio[clarification needed] technology may have UAV applications.[32]

Learning capabilities

UAVs may exploit distributed neural networks.[4]

See also

References

  1. ^ The Future of Drone Use: Opportunities and Threats from Ethical and Legal Perspectives, Asser Press – Springer, chapter by Alan McKenna, page 355
  2. ^ Kaplan, Philip (2013). Naval Aviation in the Second World War. Pen and Sword. p. 19. ISBN 978-1-4738-2997-8.
  3. ^ Taylor, John W. R.. Jane's Pocket Book of Remotely Piloted Vehicles.
  4. ^ a b c d Floreano, Dario; Wood, Robert J. (27 May 2015). "Science, technology and the future of small autonomous drones". Nature. 521 (7553): 460–466. Bibcode:2015Natur.521..460F. doi:10.1038/nature14542. PMID 26017445. S2CID 4463263.
  5. ^ Fasano, Giancarmine; Accardo, Domenico; Tirri, Anna Elena; Moccia, Antonio; De Lellis, Ettore (1 October 2015). "Radar/electro-optical data fusion for non-cooperative UAS sense and avoid". Aerospace Science and Technology. 46: 436–450. Bibcode:2015AeST...46..436F. doi:10.1016/j.ast.2015.08.010.
  6. ^ "Arduino Playground – WhatIsDegreesOfFreedom6DOF9DOF10DOF11DOF". playground.arduino.cc. Retrieved 4 February 2016.
  7. ^ Carlson, Daniel F.; Rysgaard, Søren (1 January 2018). "Adapting open-source drone autopilots for real-time iceberg observations". MethodsX. 5: 1059–1072. doi:10.1016/j.mex.2018.09.003. ISSN 2215-0161. PMC 6139390. PMID 30225206.
  8. ^ Lesko, J.; Schreiner, M.; Megyesi, D.; Kovacs, Levente (November 2019). "Pixhawk PX-4 Autopilot in Control of a Small Unmanned Airplane". 2019 Modern Safety Technologies in Transportation (MOSATT). Kosice, Slovakia: IEEE. pp. 90–93. doi:10.1109/MOSATT48908.2019.8944101. ISBN 978-1-7281-5083-3. S2CID 209695691.
  9. ^ Bristeau, Callou, Vissière, Petit (2011). "The Navigation and Control technology inside the AR.Drone micro UAV" (PDF). IFAC World Congress.{{cite web}}: CS1 maint: multiple names: authors list (link)
  10. ^ Barnard, Joseph (2007). "Small UAV Command, Control and Communication Issues" (PDF). Barnard Microsystems.
  11. ^ "The Cheap Drone Camera That Transmits to Your Phone". Bloomberg.com. Retrieved 3 February 2016.
  12. ^ "Cellular enables safer drone deployments". Qualcomm. Retrieved 9 May 2018.
  13. ^ "Identifying Critical Manned-Unmanned Teaming Skills for Unmanned Aircraft System Operators" (PDF). U.S. Army Research Institute for the Behavioral and Social Sciences. September 2012. Archived (PDF) from the original on 6 February 2016.
  14. ^ US application 20170127245, Adkins, Timothy M., "4G drone link", published 2017-05-04 , now abandoned.
  15. ^ Sharma, Navuday; Magarini, Maurizio; Jayakody, Dushantha Nalin K.; Sharma, Vishal; Li, Jun (August 2018). "On-Demand Ultra-Dense Cloud Drone Networks: Opportunities, Challenges and Benefits". IEEE Communications Magazine. 56 (8): 85–91. doi:10.1109/MCOM.2018.1701001. hdl:11311/1063273. ISSN 1558-1896. S2CID 52019723.
  16. ^ "Minimum requirements related to technical performance for IMT-2020 radio interface(s)". www.itu.int. Retrieved 8 October 2020.
  17. ^ Roberge, V.; Tarbouchi, M.; Labonte, G. (1 February 2013). "Comparison of Parallel Genetic Algorithm and Particle Swarm Optimization for Real-Time UAV Path Planning". IEEE Transactions on Industrial Informatics. 9 (1): 132–141. doi:10.1109/TII.2012.2198665. ISSN 1551-3203. S2CID 8418538.
  18. ^ Tisdale, J.; Kim, ZuWhan; Hedrick, J.K. (1 June 2009). "Autonomous UAV path planning and estimation". IEEE Robotics Automation Magazine. 16 (2): 35–42. doi:10.1109/MRA.2009.932529. ISSN 1070-9932. S2CID 9696725.
  19. ^ Cekmez, Ozsiginan, Aydin And Sahingoz (2014). "UAV Path Planning with Parallel Genetic Algorithms on CUDA Architecture" (PDF). World congress on engineering.{{cite web}}: CS1 maint: multiple names: authors list (link)
  20. ^ Davenport, Christian (23 April 2015). "Watch a step in Navy history: an autonomous drone gets refueled mid-air". The Washington Post. ISSN 0190-8286. Retrieved 3 February 2016.
  21. ^ Clough, Bruce (August 2002). "Metrics, Schmetrics! How The Heck Do You Determine A UAV's Autonomy Anyway?" (PDF). US Air Force Research Laboratory. Archived (PDF) from the original on 6 February 2016.
  22. ^ Serres, Julien R.; Masson, Guillaume P.; Ruffier, Franck; Franceschini, Nicolas (2008). "A bee in the corridor: centering and wall-following" (PDF). Naturwissenschaften. 95 (12): 1181–1187. Bibcode:2008NW.....95.1181S. doi:10.1007/s00114-008-0440-6. PMID 18813898. S2CID 226081.
  23. ^ Roca, Martínez-Sánchez, Lagüela, and Arias (2016). "Novel Aerial 3D Mapping System Based on UAV Platforms and 2D Laser Scanners". Journal of Sensors. 2016: 1–8. doi:10.1155/2016/4158370.{{cite journal}}: CS1 maint: multiple names: authors list (link)
  24. ^ "ETH Zurich: Drones with a Sense of Direction". Ascending Technologies GmbH. 10 November 2015. Retrieved 3 February 2016.
  25. ^ Timothy B. Lee (1 January 2018). "Why experts believe cheaper, better lidar is right around the corner" – via Ars Technica.
  26. ^ Shaojie Shen (16 November 2010), Autonomous Aerial Navigation in Confined Indoor Environments, retrieved 3 February 2016
  27. ^ "SWEEPER Demonstrates Wide-Angle Optical Phased Array Technology". www.darpa.mil. Retrieved 3 February 2016.
  28. ^ "LIDAR: LIDAR nears ubiquity as miniature systems proliferate". www.laserfocusworld.com. 13 October 2015. Retrieved 3 February 2016.
  29. ^ Quack, Ferrara, Gambini, Han, Keraly, Qiao, Rao, Sandborn, Zhu, Chuang, Yablonovitch, Boser, Chang-Hasnain, C. Wu (2015). "Development of an FMCW LADAR Source Chip using MEMS-Electronic-Photonic Heterogeneous Integration". University of California, Berkeley.{{cite web}}: CS1 maint: multiple names: authors list (link)
  30. ^ "DARPA's Plan to Overwhelm Enemies With Swarming Drones – Drone 360". Drone 360. 6 April 2015. Retrieved 3 February 2016.
  31. ^ NewWorldofWeapons (17 January 2014), US Air force STEALTH UAV armed with LASER GUN named General Atomics Avenger, retrieved 3 February 2016
  32. ^ Young (December 2012). "Unified Multi-domain Decision Making: Cognitive Radio and Autonomous Vehicle Convergence". Faculty of the Virginia Polytechnic Institute and State University. hdl:10919/19295. Retrieved 18 September 2020.