Amazon Technologies, Inc.

Verity Ag

Verity Studios Ag

Kiva Systems, Inc.

Eth Zurich

Perspective Robotics Ag

Raffaello D'Andrea

Markus Waibel

Michael Cordell Mountz

Markus Florian Hehn

Peter R Wurman

Michael T Barbehenn

Andrew E Hoffman

Luca Gherardi

Sergei Lupashin

Mark W Mueller

Peter K Mansfield

Patrick R Dingle

Dennis Polic

Federico Augugliaro

Philipp Reist

James Raymond Allard

Michael Harrison Decker

Fabrizio Santini

David C Koehler

Matthew E Kimmel

Burl W Amsbury

John A LaPlante

Anton Josef Ledergerber

Dennis Polle

David P Lyons, Ii

Michael D Hamer

According to a first aspect of the invention, there is provided a method for operating a multicopter experiencing a failure during flight, the multicopter comprising a body, and at least four effectors attached to the body, each operable to produce both a torque and a thrust force which can cause the multicopter to fly when not experiencing said failure. The method may comprise the step of identifying a failure wherein the failure affects the torque and/or thrust force produced by an effector, and in response to identifying a failure carrying out the following steps, (1) computing an estimate of the orientation of a primary axis of said body with respect to a predefined reference frame, wherein said primary axis is an axis about which said multicopter rotates when flying, (2) computing an estimate of the angular velocity of said multicopter, (3) controlling one or more of said at least four effectors based on said estimate of the orientation of the primary axis of said body with respect to said predefined reference frame and said estimate of the angular velocity of the multicopter. The step of controlling one or more of said at least four effectors may be performed such that (a) said one or more effectors collectively produce a torque along said primary axis and a torque perpendicular to said primary axis, wherein (i) the torque along said primary axis causes said multicopter to rotate about said primary axis, and (ii) the torque perpendicular to said primary axis causes said multicopter to move such that the orientation of said primary axis converges to a target orientation with respect to said predefined reference frame, and (b) such that said one or more effectors individually produce a thrust force along said primary axis.

Controlled flight of a multicopter experiencing a failure affecting an effector

A self-localizing apparatus uses timestampable signals transmitted by transceivers that are a part of a distributed localization system to compute its position relative to the transceivers. Transceivers and self-localizing apparatuses are arranged for highly accurate timestamping using digital and analog reception and transmission electronics as well as one or more highly accurate clocks, compensation units, localization units, position calibration units, scheduling units, or synchronization units. Transceivers and self-localizing apparatuses are further arranged to allow full scalability in the number of self-localizing apparatuses and to allow robust self-localization with latencies and update rates useful for high performance applications such as autonomous mobile robot control.

Distributed localization systems and methods and self-localizing apparatus

The invention relates to a method and device for estimating angle information () of a received ultra-wideband wireless signal. Upon reception of a wireless signal emitted from a transmitting device () with known sounding sequence, the receiving device () estimates the channel impulse response (CIR), selects a portion of the channel impulse response (CIR), and estimates angle information () given the angle-dependent antenna transfer functions of either the transmitting device (), the receiving device (), or both. For this, the selected portion of the channel impulse response of the signal is fed into a neural network () which outputs an angle information probability distribution for the ultra-wideband wireless signal ().

Angle information estimation of ultra-wideband wireless signals

Localization systems and methods for transmitting timestampable localization signals from anchors according to one or more transmission schedules. The transmission schedules may be generated and updated to achieve desired positioning performance. For example, one or more anchors may transmit localization signals at a different rate than other anchors, the anchor transmission order can be changed, and the signals can partially overlap. In addition, different transmission parameters may be used to transmit two localization signals at the same time without interference. A self-localizing apparatus is able to receive the localization signals and determine its position. The self-localizing apparatus may have a configurable receiver that can select to receive one of multiple available localization signals. The self-localizing apparatuses may have a pair of receivers able to receive two localization signals at the same time. A bridge anchor may be provided to enable a self-localizing apparatus to seamlessly transition between two localization systems.

Methods and systems for scheduling the transmission of localization signals and operating self-localizing apparatus

According to the present invention there is provided an aerial vehicle that is operable to fly, the aerial vehicle having at least a first and second subsystem that are operably connected, wherein the first subsystem comprises a first flight module, first one or more effectors that are selectively operable to generate a first force sufficient to cause the aerial vehicle to fly; and the second subsystem comprises a second flight module, second one or more effectors that are selectively operable to generate a second force sufficient to cause the aerial vehicle to fly; such that the first or second subsystem can be selectively used to fly the aerial vehicle not relying on the one or more effectors of the other subsystem. There is further provided a corresponding method for controlling an aerial vehicle.

Aerial vehicle

A system comprising, a plurality of unmanned aerial vehicles and a single controller for controlling said plurality of unmanned aerial vehicles, wherein the single controller is configured such that it can broadcast a command to all of the plurality of unmanned aerial vehicles so that each of the plurality of unmanned aerial vehicles receive the same command; and wherein each of the unmanned aerial vehicles comprise a memory which stores a plurality of predefined flight paths each of which is assigned to a respective command; and wherein each of the unmanned aerial vehicles comprise a processor which can, (i) receive a command which has been broadcasted by the single controller to said plurality of unmanned aerial vehicles, (ii) retrieve from the memory of that aerial vehicle the flight path which is assigned in the memory to that command, and (iii) operate the aerial vehicle to follow the retrieved flight path. There is further provided a corresponding method of controlling a plurality of unmanned aerial vehicles.

System having a plurality of unmanned aerial vehicles and a method of controlling a plurality of unmanned aerial vehicles

A flying machine storage container is provided that comprises multiple charging stations and a clamping mechanism. The clamping mechanism is configured to secure flying machines in the charging stations and securely close charging circuits between the storage container and the flying machines. A system for launching flying machines is also provided. The system comprises two regions and a transition region between the two regions. The two regions each constrain the positioning of a flying machine and the transition region enables a flying machine to move from the first region to the second region to reach an exit. A flying machine having sufficient performance capabilities will be able to successfully launch. Centralized and decentralized communication architectures are also provided for communicating data between a central control system, multiple storage containers, and multiple stored flying machines stored at each of the storage containers.

Systems and methods for charging, transporting, and operating flying machines

A transceiver network comprises first, second, and third transceivers that are configured to transmit signals that are spread over a bandwidth that exceeds the lesser of 125 MHz and 5% of an arithmetic center frequency of the signals. An additional transceiver with at least a partially unknown relative position can be added to the transceiver network. The additional transceiver receives the signals from the first, second, and third transceivers and timestamps the receptions. A position calibration unit is configured to compute the position of the additional transceiver relative to the first, second, and third transceivers based on the reception timestamps and known relative locations of the first, second, and third transceivers. The additional transceiver can be configured to transmit (e.g., in a transmission time slot) an additional signal as part of the transceiver network.

According to a first aspect of the present invention there is provided an arrangement comprising, a volitant body comprising at least one actuator; a control unit for controlling said actuator; and a mechanical arrangement for operationally connecting said volitant body to a reference point remote from said volitant body. There is further provided a corresponding method for operating such an arrangement.

Flying camera with string assembly for localization and interaction

Growing community of inventors

Wollerau, Switzerland

Raffaello D'Andrea