Abstract: Systems and methods may use a drone swarm to increase cargo capacity. A drone swarm may include a networked drone system or two or more drones, such as a parent drone and a child drone. A method may include receiving support component balance information captured by an inertial measurement unit on the support component supported by a parent drone, adjusting movement of the parent drone according to a control system using the support component balance information, receiving an indication of a low battery in a drone in the networked drone system, the indication including an identification of a replacement drone to replace the drone with the low battery in the networked drone system, and sending a reconfiguration command to at least one child drone to incorporate the replacement drone in the networked drone system.

Abstract: Embodiments of methods and apparatus for close formation flight are provided herein. In some embodiments, a method for establishing situational awareness during formation flight includes exchanging transponder signals between at least two aircraft, establishing two-way communication links between the at least two aircraft, exchanging telemetry data between the at least two aircraft, and assigning the roles of a leader and a follower to the aircraft.

Abstract: A system and method for participating in a multi-USV performance in three-dimensional space. The USV can include: a computer processor; a sensory device configured to detect live sensory information relative to a second USV participating in the performance in proximity to the USV; and a spatial control module executing on the computer processor and configured to enable the computer processor to: (i) receive instructions for performing a pre-determined sequence of spatial maneuvers of the performance; (ii) begin execution of the pre-determined sequence of spatial maneuvers according to the instructions; (iii) identify a modified sequence of spatial maneuvers calculated based on the live sensory information from the sensory device; (iv) halt execution of the pre-determined sequence of spatial maneuvers; and/or (v) execute the modified sequence of spatial maneuvers.

Abstract: Various embodiments are generally directed to identity verification using autonomous vehicles. A security policy may be used to determine when identity verification using autonomous vehicles is required. The autonomous vehicle may be deployed to a location to verify the identity of the user based on one or more of images, audio data, biometric data, and wireless data connections.

Abstract: A method for inspecting a solar panel of a solar power station is performed in a controller for an unmanned aerial vehicle, UAV, and includes the steps of: receiving an inspection request for a subset of the solar panels navigating, in a first stage, using radio signals, the UAV to an initial location in a vicinity of a particular solar panel of the subset of solar panels; positioning, in a second stage, the UAV using at least one near field sensor of the UAV; and capturing, using the infrared camera, an image of the particular solar panel.

Abstract: Disclosed herein is a system and method for drone connectivity using cellular networks for out of line-of-sight applications and tracking drones during flight. The present invention may be modular, allowing users to program customizable modes for one or more microprocessors of the system. In one embodiment, a system comprises a drone configured with a processor, a cellular modem and a flight controller, the processor connected to the cellular modem and connected to the flight controller via serial connections; a cloud server; a remote control device, and wherein the system is configured for communication from the remote control device to the cloud server via internet communication, and from the cloud server to the drone via a cellular network in communication with the cloud server and the cellular modem, the system providing a communication network for the delivery and routing of data between the remote control device and the drone.

Abstract: A system to maintain a phase difference is disclosed. Two or more aircraft fly in a continuous periodic trajectory. The system maintains a phase difference between the two or more aircraft. Telemetry information for a reference aircraft moving in a first periodic trajectory is received. A phase difference between a primary aircraft and the reference aircraft with respect to the first periodic trajectory is determined. A variance in the phase difference between the primary aircraft and the reference aircraft from the target phase difference is determined. A new trajectory for the primary aircraft that decreases the variance in the phase difference with respect to the new periodic trajectory is determined, and the primary aircraft is maneuvered to follow the new trajectory.

Abstract: Dynamic analysis and updating real-time restrictions for remote controlled vehicles. Remote controlled vehicles are subject to geospatial restrictions that are updated in real time; dynamic analysis of geospatial restrictions allows for proper operation of a remote controlled vehicle.

Abstract: Systems and methods are provided for least one leading drone configured to move to a leading drone future location based on a future location of a base station. A set of base station future locations may form a base station path for the base station to traverse. Also, a set of leading drone future locations may form a leading drone path for the leading drone to traverse. The base station's future location may be anticipated from a prediction or a predetermination. The leading drone, navigating along the leading drone path, may collect sensor data and/or perform tasks. Accordingly, the leading drone may move ahead of the base station in motion, as opposed to following or remaining with the base station.

Abstract: Methods and systems for real-time video-based multiplayer gaming environments enable operators to remotely control vehicles over a network comprising a base station and a server. Cameras may record and transmit encoded video relating to the vehicles for display at a remote console. In response, the operator is able to input commands to remotely control the operation of the vehicle.

Abstract: The present invention relates to electro-optic guided missile systems and, in particular, it concerns systems and methods providing enhanced navigation capabilities based on ego-motion processing of seeker images. The missile system comprising: a missile; a seeker located at a nose portion of said missile, said seeker comprising an electro-optic imaging sensor; and a control arrangement for steering the missile along a flight path to a target, characterized in that the missile system further comprises: a navigation subsystem receiving images from said imaging sensor, said navigation subsystem being configured to: co-process a plurality of said images from said imaging sensor to derive ego-motion of said missile relative to a region viewed by said imaging sensor; derive from said ego-motion a calculated target direction from said missile to a target.

Abstract: Various embodiments provide methods for controlling landings of a UAV in a landing zone including a plurality of landing bays. Various embodiments include a method implemented on a computing device for receiving continuous real-time sensor data from a transceiver and from sensors onboard the UAV, and detecting a target landing bay within the plurality of landing bays within the landing zone that is available for landing based on the continuous real-time sensor data. Orientation and position coordinates for landing in the target landing bay may be calculated based on the continuous real-time sensor data. Information regarding positions and flight vectors of a plurality of autonomous UAVs may be obtained, and a flight plan for landing in the target landing bay may be generated based on the orientation and the position coordinates, positions and flight vectors of the plurality of autonomous UAVs and a current orientation and position of the UAV.

Abstract: The aircraft (10) includes: at least one electric motor (135); at least one stand-alone electrical power supply (110, 120) supplying power to the electric motor; propulsion elements (130) referred to as “auxiliary propulsion elements”, included in the group including: a stand-alone electrical power supply (130) supplying power to the electric motor, a power supply converting thermal energy into electrical energy and supplying power to the electric motor, and an internal combustion engine; and a structure (100) configured to integrate each electric motor, each stand-alone electrical power supply and the auxiliary propulsion elements, the parameters of the structure being substantially identical regardless of the auxiliary propulsion elements. A method of fitting out such an aircraft is also described.

Abstract: Methods and systems for real-time video-based multiplayer gaming environments enable operators to remotely control vehicles over a network comprising a base station and a server. Cameras may record and transmit encoded video relating to the vehicles for display at a remote console. In response, the operator is able to input commands to remotely control the operation of the vehicle.

Abstract: A method and device used to improve flying education, and reduce pilot student hazard when passing from simulators to the real aircraft, by introducing an intermediary stage where a simulator and a model radio-controlled aircraft with similar features as original is used in a system with many participants, an instructor, flight monitors, command center, mission control, audience located remotely and taking part in the same action via internet telecommunication. The simulator is used to measure biometric parameters of the pilots, certify them, and also for gaming, having fail-safe procedures embedded. System contains a flight-monitoring network, using both goniometry and radar devices, placed on surface and airborne, using these devices as signal repeaters for extensions of communication. The system may be used in missions dangerous to human crews, and by the complexity of simulation it improves the flying, as well as to improve the piloting of RC aircrafts.

Abstract: An electronic system for stabilizing steering of a model vehicle may provide a curvature steering control of an RC vehicle. The approximate curvature control of the RC vehicle determined using error integration to achieve full steering. Application of a leaky integrator may be used to minimize steering memory. The leak factor may be based off gain scheduling of the steering input.

Abstract: In an approach to hazard detection, one or more computer processors receive a request from a first vehicle user for assistance from an unmanned aerial vehicle (UAV). The one or more computer processors locate a UAV. The one or more computer processors determine the location of the first vehicle. The one or more computer processors deploy the UAV to the location of the first vehicle. The one or more computer processors determine whether one or more hazards associated with a path of the first vehicle are detected.

Abstract: Innovative new systems and method of operating the systems, wherein the system comprises an airborne platform comprising an unmanned balloon; a payload that is separate from the unmanned balloon; a transceiver; first and second flight termination devices; at least two separate power sources for the first and second flight termination devices; a sensor; a processor; a pump; a valve; and a tether that when broken separates the unmanned balloon and the payload, are disclosed herein.

Abstract: An unmanned aerial vehicle includes at least one rotor motor configured to drive at least one propeller to rotate. The unmanned aerial vehicle includes a data center including a processor; a data storage component; and a wireless communications component. The unmanned aerial vehicle includes a hybrid generator system configured to provide power to the at least one rotor motor and to the data center, the hybrid generator system including a rechargeable battery configured to provide power to the at least one rotor motor; an engine configured to generate mechanical power; and a generator motor coupled to the engine and configured to generate electrical power from the mechanical power generated by the engine. The data center may include an intelligent data management module configured to control power distribution and execution of mission tasks in response to available power generation and mission task priorities.

Abstract: A remote control device, method, and system for controlling a stabilized camera remotely are disclosed. The remote control device includes a steering member rotatable around a pan axis, a tilt axis, and/or a roll axis of the remote control device, an inertial measurement unit (IMU) mounted on the steering member and configured to measure a pointing direction of the steering member in relation to the pan axis, the tilt axis, and/or the roll axis, a controller configured to derive a pointing direction update based on the measurements obtained by the IMU, and a transmitter configured to transmit, to a stabilization system configured to stabilize the camera in accordance with a commanded pointing direction, the derived pointing direction update as the commanded pointing direction to effectuate adjustment of a pointing direction of the camera to follow a rotational movement of the steering member.

Abstract: Disclosed are a mobile terminal and a method for controlling the same. The mobile terminal which wirelessly communicates with an unmanned aircraft including a camera, includes a wireless communication unit configured to receive a capturing image including a plurality of images captured by the camera; a memory configured to store flight information of the unmanned aircraft corresponding to each of the plurality of images; a display unit configured to output the captured image; and a controller configured to transmit a flight control command which is formed by flight information corresponding to at least one image to the unmanned aircraft, based on a recapturing command to at least one image among the plurality of images.

Abstract: Disclosed herein is a drone docking station for deposit of items delivered by drone. Items may include food items, groceries, parcels and others. A secure porch, roof, window or otherwise building mounted box may be secured through to an existing edifice or may be configured to mount to an existing mailbox post. The basic elements making up the components of the box enable it to carry out efficient and secure delivery of goods to a container box located at a specific address and to securely hold those goods until they are picked-up regardless of duration, weather, or otherwise. The drone dock may employ different technological devices to provide for communication between the drone docking station and a drone to provide security and preservation of the delivered goods before during and after delivery.

Abstract: Systems and methods are provided for a network of relay drones utilized as a set of relays or linkages between a base station and a working drone controlled by the base station. The relay drones in the network may augment a communication link or communication signal between the base station and working drone. Relay drones may augment the communication link by acting as nodes that relay communication between the base station and the working drone by boosting the communication signal at each node to compensate for loss of signal power over a traveled distance and/or providing a path with a direct line of sight between the base station and working drone. Directional antennas may be utilized when a direct line of sight is established, which may improve communication signal efficacy when compared with omnidirectional antennas.

Abstract: A system and method for optical communication between multiple UUVs, more specifically, for leader-follower formations between UUVs. The system focuses on the characterization and modeling of a 1-dimensional and/or 3-dimensional light field produced from a light source mounted on a Leader UUV, which is detected by one or more follower UUVs. Communication algorithms are used to monitor the UUV's motion and orientation utilizing simulators, look up tables, and the like. A variety of detectors arrays can be used in a variety of wavelengths depending on the desired application.

Abstract: Described is an airborne monitoring station (“AMS”) for use in monitoring a coverage area and/or unmanned aerial vehicles (“UAVs”) positioned within a coverage area of the AMS. For example, the AMS may be an airship that remains at a high altitude (e.g., 45,000 feet) that monitors a coverage area that is within a line-of-sight of the AMS. As UAVs enter, navigate within and exit the coverage area, the AMS may wirelessly communicate with the UAVs, facilitate communication between the UAVs and one or more remote computing resources, and/or monitor a position of the UAVs.

Abstract: The system comprises a drone and a ground station with a console adapted to be directed towards the drone, and virtual reality glasses rendering images taken by a camera of the drone. The system further comprises means for modifying the framing of the images taken by the camera as a function of framing instructions received from the ground station. It further comprises relative heading determination means (302-324) for periodically elaborating an angular difference between the orientation of the glasses and the orientation of the console, and means (316) for elaborating framing instructions for the drone as a function said angular difference. The sudden changes of framing when the user simply turns the console and his whole body, head included, towards the drone to follow it in its displacements, are hence avoided.

Abstract: A combined radar and telemetry system is described. The combined radar and telemetry system includes a processing unit that executes instructions, where the instructions define a radar waveform and a telemetry waveform. The processor outputs a digital baseband signal based upon the instructions, where the digital baseband signal is based upon the radar waveform and the telemetry waveform. A radar and telemetry circuit transmits, simultaneously, a radar signal and telemetry signal based upon the digital baseband signal.

Abstract: An unmanned vehicle determines how to perform a task based at least in part on a message received from another unmanned vehicle. At a later time, the unmanned vehicle detects that the other unmanned vehicle has become untrusted. The unmanned vehicle recalculates how to perform the task such that the recalculation is independent of any messages from the other unmanned vehicle. The unmanned vehicle may also transmit messages to other unmanned vehicles to provide notification of untrustworthiness of the other unmanned vehicle.

Abstract: This unit implements a remote-control console (20) supporting a tablet (18). The console comprises a TX/RX module (48) interfaced with a TX/RX module (50) of the tablet to form a first Wi-Fi local network, which is a short-range standard network. The console comprises another specific TX/RX module (54), interfaced with an TX/RX module (58) of the drone (10) to form a second Wi-Fi local network, which is an optimized long-range network, both being networks operating on non-shared channels. A bidirectional routing module (78) ensures the interfacing between the two Wi-Fi networks, to allow the transparent exchange of data between the drone (10) and the tablet (18), as well as with levers and buttons of the console (64, 66) or with a peripheral (80) connected thereto.

Abstract: A method, system, and recording medium including a mission receiving device configured to receive a mission for the drone-swarm based on a user input, a drone and pattern recruiting device configured to recruit a plurality of drones based on the mission, and a flocking goal device configured to arrange the plurality of drones in the drone-swarm in a pattern to satisfy the mission.

Abstract: In at least some implementations, an aircraft includes a fuselage, a wing spar rotatably carried by the fuselage, a first wing element and a second wing element. The first wing element is carried by the wing spar, rotatable with the wing spar, and slidably moveable relative to the fuselage and wing spar. The second wing element is connected to the first wing element for pivoted movement of the second wing element relative to the first wing element. The second wing element at least partially overlaps the first wing element and the first and second wing elements are moveable to a plurality of positions wherein the amount that the second wing element overlaps the first wing element varies to vary the effective combined wing area of the wing elements.

Abstract: An unmanned aerial vehicle (UAV) carries a camera, sends data from the camera, and receives commands. The UAV is connected to a messaging platform. Pictures or video clips received from the UAV are selected and placed in messages broadcast by an account associated with the UAV. Video footage from the camera is live-streamed in a card-type message. Account holders of the messaging platform may control the UAV with commands embedded in messages and directed towards an account associated with the UAV. Controllable elements of the UAV include UAV location, camera orientation, camera subject, UAV-mounted lighting, a UAV-mounted display, a UAV-mounted projector, UAV-mounted speakers, and a detachable payload. UAV control may be determined through democratic means. Some UAV functionality may be triggered through aggregated engagements on the messaging platform. The UAV may include a display screen and/or a microphone to provide for telepresence or interview functionality.

Abstract: Described herein is a control system that facilitates assistance mode(s). In particular, the control system may determine a particular assistance mode associated with an account. This particular assistance mode may specify (i) operations for an aerial vehicle to carry out in order to obtain sensor data providing environment information corresponding to a location associated with the account and (ii) feedback processes to provide feedback, via a feedback system associated with the account, that corresponds to respective environment information. The control system may transmit to the aerial vehicle an indication of the particular operations corresponding to the particular assistance mode and may then receive environment information for the location associated with the account. Based on the received environment information, the control system may apply the specified feedback processes to initiate feedback in accordance with the particular assistance mode via the associated feedback system.

Abstract: A radio controlled (RC) vehicle includes a receiver that is coupled to receive an RF signal from a remote control device, the RF signal containing command data in accordance with a first coordinate system, wherein the first coordinate system is from a perspective of the remote control device. A motion sensing module generates motion data based on the motion of the RC vehicle. A processing module transforms the command data into control data in accordance with a second coordinate system, wherein the second coordinate system is from a perspective of the RC vehicle. A plurality of control devices control the motion of the RC vehicle based on the control data.

Abstract: A motion sensing remote control device including a motion sensing module, a calculation unit, a motion setting unit, a transmit unit and a receiving unit is disclosed. The present invention controls a remote control car to perform various motions by sensing the user's gestures. The motion sensing module senses and converts the gestures into a voltage signal for the calculation unit to perform calculation. The motion setting unit generates a corresponding command based on the calculation result of the calculation unit, and transmits the command to the remote control car through the transmit unit and the receiving unit such that the remote control car executes the received command to perform the corresponding motion specified by the user.

Abstract: The invention is directed toward a system and method for placing, activating, and testing sensors. The system comprises one or more server computers, one or more communication hubs, one or more unmanned aerial vehicles, and one or more sensors. The method comprises the steps of receiving geographic sensor placement locations, receiving sensor parameters, determining the geographic location of sensors, respectively sending location query signals to the unmanned aerial vehicles, respectively receiving location reply signals from the unmanned aerial vehicles, and calculating a geographic flight path for the unmanned aerial vehicles. The method also comprises calculating mission objectives and the energy needs of the unmanned aerial vehicles to complete the mission objectives. The method then determines the most efficient combination of unmanned aerial vehicles to complete the mission objectives and assigns the tasks to the unmanned aerial vehicles.

Abstract: The method and system may be used to control the movement of a remote aerial device in an incremental step manner during a close inspection of an object or other subject matter. At the inspection location, a control module “stabilizes” the remote aerial device in a maintained, consistent hover while maintaining a close distance to the desired object. The control module may retrieve proximal sensor data that indicates possible nearby obstructions to the remote aerial device and may transmit the data to a remote control client. The remote control module may determine and display the possible one or more non-obstructed directions that the remote aerial device is capable of moving by an incremental distance. In response to receiving a selection of one of the directions, the remote control module may transmit the selection to the remote aerial device to indicate the next movement for the remote aerial device.

Abstract: Remote controllers and systems thereof are disclosed. The remote controller remotely operates a receiving host, in which the receiving host provides voice input and speech recognition functions. The remote controller comprises a first input unit and a second input unit for generating a voice input request and a speech recognition request. The generated voice input and speech recognition requests are then sent to the receiving host, thereby forcing the receiving host to perform the voice input and speech recognition functions.

Abstract: Systems and methods for use in navigating aircraft are provided. A method includes transmitting messages from a plurality of aircraft within time slots of a data transmission using a data link radio of each of the aircraft. The time slots of the data transmission are divided by time. The master aircraft transmits a message within a first time slot. Each message includes position data, time data, aircraft orientation data, and intended flight path data for the aircraft transmitting the message. The method further includes, for each of the plurality of aircraft, receiving a plurality of received messages transmitted by the other aircraft within the data transmission, and generating a representation of an environment around the aircraft based on the data within the received messages. The representation includes a current position and an intended path for one or more of the other aircraft.

Abstract: A vision-based automatic recovery method including steps of: generating a reference trajectory connecting an align point and a recovery point that is provided through wireless communication; taking an image containing a target through a front vision camera, determining a position and a size of the target in the taken image, and calculating a distance between the target and the unmanned aerial vehicle; generating an attitude command for changing a direction of the unmanned aerial vehicle so as to center the target in an image taken by the front vision camera; and generating a virtual trajectory by combining the generated reference trajectory and the generated attitude command, a weight of the attitude command being increased as the unmanned aerial vehicle moving from the align point to the recovery point.

Abstract: Devices, systems, and methods for social behavior of a telepresence robot are disclosed herein. A telepresence robot may include a drive system, a control system, an object detection system, and a social behaviors component. The drive system is configured to move the telepresence robot. The control system is configured to control the drive system to drive the telepresence robot around a work area. The object detection system is configured to detect a human in proximity to the telepresence robot. The social behaviors component is configured to provide instructions to the control system to cause the telepresence robot to operate according to a first set of rules when a presence of one or more humans is not detected and operate according to a second set of rules when the presence of one or more humans is detected.

Abstract: Embodiments are directed to receiving, by a control station, an input including a command for re-location of a vehicle from a first location to a second location, the input identifying the second location, determining, by the control station, at least one of a distance, a direction, an altitude, and a latitude and longitude for the vehicle to travel from the first location to the second location, and transmitting, by the control station, the command and the at least one of a distance, a direction, an altitude, and a latitude and longitude to the vehicle.

Abstract: A radio controlled UAV is disclosed. The UAV includes a parachute, with a cylindrical power and control module suspended vertically below the parachute. In one embodiment, a propulsion source is mounted on top of the power and control module with control lines connected to the module below the propulsion source, and in another embodiment the power and control module is suspended from a point above a propulsion source. The UAV is controlled by radio controls from a hand held controller, with actuators retracting and letting out control lines attached to the parachute in order to control direction of the parachute. The UAV may be launched from a tube using a pressurized tank with a nozzle expelling gas from the tank, the tank and nozzle towing a canister from which the UAV is deployed.

Abstract: A remotely-piloted aircraft for distributing beneficial insects on a target area is provided. The aircraft includes an enclosure, including a top lid, one or more internal compartments, a door for each of the one or more internal compartments, and an actuator to open and close each of the doors. The aircraft also includes a circuit to control the actuators, a wireless receiver, coupled to the circuit, to receive commands to open and close the doors, and one or more power sources to power the actuators and the wireless receiver. An operator controls the aircraft and the circuit with at least one of a wireless transmitter and an uploaded program in the circuit. When the wireless receiver receives a command to open a door, the circuit controls an actuator corresponding to the door. The actuator opens the door, and the beneficial insects are distributed from internal compartments.

Abstract: A system and method of coordination of aerial vehicles through a central server are disclosed. In one embodiment, a system includes a central server and an Internet protocol network. A first aerial vehicle is communicatively coupled with the central server through the Internet protocol network and a second aerial vehicle is communicatively coupled with the first aerial vehicle when a command is transferred through the central server using the Internet protocol network. A first computing device of a first user of the first aerial vehicle operatively controls the first aerial vehicle and a second computing device of a second user of the second aerial vehicle operatively controls the second aerial vehicle. At least one of the first computing device of the first user and the second computing device of the second user communicate the command to the first aerial vehicle through the central server.

Abstract: The present invention provides methods and apparatus for unmanned aerial vehicles (UAVs) with improved reliability. According to one aspect of the invention, interference experienced by onboard sensors from onboard electrical components is reduced. According to another aspect of the invention, user-configuration or assembly of electrical components is minimized to reduce user errors.

Abstract: The drone comprises altitude determination means (134), with an estimator (152) combining the measures of an ultrasound telemetry sensor (154) and of a barometric sensor (156) to deliver an absolute altitude value of the drone in a terrestrial system. The estimator comprises a predictive filter (152) incorporating a representation of a dynamic model of the drone making it possible to predict the altitude based on the motor commands (158) and to periodically readjust this prediction as a function of the signals delivered by the telemetry sensor (154) and the barometric sensor (156). Validation means analyze the reflected echoes and possibly modify the parameters of the estimator and/or allow or invalidate the signals of the telemetry sensor. The echo analysis also makes it possible to deduce the presence and the configuration of an obstacle within the operating range of the telemetry sensor, to apply if need be a suitable corrective action.

Abstract: A method for retrieving personnel is provided. The method includes receiving a radio signal indicating a real-time position of personnel to be retrieved, deploying an unmanned aerial vehicle to the real-time position, receiving an indication that the personnel to be retrieved is on-board the unmanned aerial vehicle, and operating the unmanned aerial vehicle to move the personnel to a different location.

Abstract: An illustrative emergency-support system may include multiple unmanned aerial vehicles (UAVs), which are configured to provide emergency support for a number of different emergency situations. Further, the emergency-support system may be configured to: (a) identify a request for assistance in a remote emergency situation, (b) identify a remote device associated with the request for assistance, (c) determine a target location corresponding to the emergency situation, (d) control a UAV to travel to the target location to provide emergency support, and (e) enable an otherwise restricted capability of one or more of the remote device or the UAV after controlling the UAV to travel to the target location, wherein the capability is enabled to help provide emergency support in the remote emergency situation.

Abstract: The appliance includes a touch screen and wireless data transmission implementation for communicating with the drone. Drone piloting commands are activated by fingers contacting and/or moving over locations of corresponding piloting symbols displayed on the screen. The method proceeds by: detecting finger contact at an arbitrary contact point in at least one predefined zone of the screen on which piloting symbols are not already displayed; displaying a piloting icon on the screen at the contact point, the piloting icon including a movable icon displayed at a position that tracks any movement of the finger contact point over the screen from an initial position to an offset position; detecting the movement of the movable icon; on detecting the movement, analyzing the direction and/or the amplitude of the movement relative to the initial position; and activating a piloting command as a function of the result of the analysis.