Abstract: A vehicle includes a body and at least one propulsion unit operatively coupled to the body. The vehicle also includes an electrical power system at least partially disposed within the body. The electrical power system includes a rechargeable battery and a health management unit operatively coupled to the rechargeable battery. The health management unit includes a state of health module configured to output information corresponding to battery health based on received battery-related data. The battery-related data includes data collected in real time operation of the rechargeable battery and battery relevant fault history of the vehicle.

Abstract: A method includes positioning a vehicle on a vehicle base station such that a first payload is aligned with an aperture in the vehicle base station. The method includes aligning an empty docking station of a payload advancing assembly with the aperture. The method includes removing the first payload from the vehicle and placing the first payload in the empty docking station of the payload advancing assembly, where the full docking station includes a second payload. The method also includes aligning a full docking station of the payload advancing assembly with the aperture and securing the second payload to the vehicle.

Abstract: Described herein is an apparatus for semi-autonomous vehicle control of a vehicle includes a distributed mission module configured to modify a mission element of a group mission based on availability of data. The group mission involves a plurality of vehicles. The apparatus also includes a guidance module configured to compute a path for a local vehicle of the plurality of vehicles based on the modified mission element. The path is configured to achieve the modified mission element. Additionally, the apparatus includes a multi-protocol translator module configured to convert the path into one or more control commands for the local vehicle. The distributed mission module, guidance module, and multi-protocol translator are located on-board the vehicle.

Abstract: A system and methods for mission re-planning are presented. Vehicles are monitored in real-time, and an incapacitated vehicle from among the vehicles that performs an incomplete task is detected. A remaining coverage set comprising a remaining coverage area for each of the vehicles is determined. A travel distance from a task completion location of each of the vehicles to a stopped point of the incapacitated vehicle is calculated to provide a travel set. An extra coverage set is determined based on the travel set and the remaining coverage set, and an incomplete coverage area for the incomplete task is calculated. The extra coverage set is compared to the incomplete coverage area and the remaining coverage area to provide a sufficiency list, and an assigned vehicle is selected from the vehicles based on the sufficiency list.

Abstract: Described herein is an apparatus for semi-autonomous vehicle control of a vehicle includes a distributed mission module configured to modify a mission element of a group mission based on availability of data. The group mission involves a plurality of vehicles. The apparatus also includes a guidance module configured to compute a path for a local vehicle of the plurality of vehicles based on the modified mission element. The path is configured to achieve the modified mission element. Additionally, the apparatus includes a multi-protocol translator module configured to convert the path into one or more control commands for the local vehicle. The distributed mission module, guidance module, and multi-protocol translator are located on-board the vehicle.

Abstract: A system for monitoring a vehicle having systems, components, and sensors has a nominal controller and an adaptive controller. A vehicle health function module is coupled to an output of the adaptive controller and generates a vehicle health output signal indicating a prognosis of at least one of the systems or components degradation of the vehicle.

Abstract: A vehicle includes a body and at least one propulsion unit operatively coupled to the body. The vehicle also includes an electrical power system at least partially disposed within the body. The electrical power system includes a rechargeable battery and a health management unit operatively coupled to the rechargeable battery. The health management unit includes a state of health module configured to output information corresponding to battery health based on received battery-related data. The battery-related data includes data collected in real time operation of the rechargeable battery and battery relevant fault history of the vehicle.

Abstract: A method includes positioning a vehicle on a vehicle base station such that a first payload is aligned with an aperture in the vehicle base station. The method includes aligning an empty docking station of a payload advancing assembly with the aperture. The method includes removing the first payload from the vehicle and placing the first payload in the empty docking station of the payload advancing assembly, where the full docking station includes a second payload. The method also includes aligning a full docking station of the payload advancing assembly with the aperture and securing the second payload to the vehicle.

Abstract: A system to load and unload material from a vehicle comprises a vehicle base station and an assembly to autonomously load and unload material from the vehicle.

Abstract: Systems and methods for health management of rechargeable batteries are disclosed. In one embodiment, a rechargeable battery system includes a rechargeable battery, and a battery health management unit operatively coupled to the rechargeable battery and including a state of health module configured to estimate a battery health by receiving battery-related data and predicting one or more failure modes. The state of health module may further include a prognostic failure mode component configured to combine at least one flight data variable with at least one model-based prognostic. In alternate embodiments, the battery health management unit may further include a state of life module and a state of charge module.

Abstract: A damage-detection apparatus for an aircraft may include a composite structure comprising embedded conductive traces. The embedded conductive traces may be for transmitting a damage-detection signal to indicate if the composite structure has been damaged.

Abstract: A vehicle base station comprises a platform on which a vehicle may be positioned, a first battery bay located on a first side of the platform, a battery replacement assembly to remove a battery from the vehicle and to replace the battery with a new battery, and a power source adapted to provide power to the vehicle while the vehicle is positioned on the platform.

Abstract: A method of testing a component of a mobile platform without using an aircraft control system of the mobile platform, where the component forms a part of the aircraft control system. The method may involve using a test controller independent of the aircraft control system to initiate a test operation. The test operation is used to generate a test signal. The test signal is applied to a test subsystem carried on the mobile platform but operable independent of the aircraft control system. The test subsystem is used to act on the component of the aircraft control system. A response of the component may then be evaluated.

Abstract: An unmanned vehicle is provided. The unmanned vehicle includes a navigation system configured to navigate the unmanned vehicle relative to a beam of energy emitted from a beam source, a power receiver configured to receive energy from the beam, and an energy storage system configured to store received energy for use in selectively powering the unmanned vehicle.

Abstract: A system and methods for mission re-planning are presented. Vehicles are monitored in real-time, and an incapacitated vehicle from among the vehicles that performs an incomplete task is detected. A remaining coverage set comprising a remaining coverage area for each of the vehicles is determined. A travel distance from a task completion location of each of the vehicles to a stopped point of the incapacitated vehicle is calculated to provide a travel set. An extra coverage set is determined based on the travel set and the remaining coverage set, and an incomplete coverage area for the incomplete task is calculated. The extra coverage set is compared to the incomplete coverage area and the remaining coverage area to provide a sufficiency list, and an assigned vehicle is selected from the vehicles based on the sufficiency list.

Abstract: A mission planning system for determining an optimum use of a plurality of vehicles in searching a predefined geographic area (PGA). A discretizer subsystem may be used for sensing the capabilities of each vehicle to produce a point set defining a number of points within the PGA that the vehicles must traverse to completely search the PGA. A task allocator subsystem may determine an optimum division of the PGA into different subregions to be handled by specific ones of the vehicles, thus to minimize an overall time needed to search the PGA. A path optimizer subsystem may determine an optimum path through a particular vehicle's assigned subregion to minimize the time needed for each specific vehicle to traverse its associated subregion.

Abstract: Systems and methods for health monitoring of complex systems are disclosed. In one embodiment, a method includes receiving a plurality of signals indicative of observation states of plurality of operating variables, performing a combined probability analysis of the plurality of signals using a diagnostic model of a monitored system to provide a health prognosis of the monitored system, and providing an indication of the health prognosis of the monitored system. In some embodiments, the monitored system may be an onboard system of an aircraft.

Abstract: A system and methods for life optimal power management of a distributed or centralized battery network system for use in aircraft functions and subsystems are disclosed. The method determines power priority of the subsystems, and selectively distributes power from the battery network system to the subsystems based on the power priority. Concurrently with distributing power, the method manages the energy in the battery network system. To determine whether the battery power is sufficient for aircraft functions, the method also computes and indicates the actual available energy left in the battery network systems. With this approach, the system and methods can provide a persistent power supply in the event an unexpected battery failure occurs, thereby enabling the aircraft to safely maintain flight operability despite a battery failure.

Abstract: A method of inspecting an aircraft. A plurality of heterogeneous unmanned vehicles are used to perform an inspection of the aircraft, each unmanned vehicle having one or more sensors. A plurality of portions of the aircraft are assigned to the vehicles for inspection based on functional capability of each vehicle. The unmanned vehicles are configured to cooperatively use the sensors to perform the inspection.

Abstract: A system and method for dividing a predefined search region into a map of a plurality of subregions to be searched by a plurality of mobile platforms, taking into account the capabilities of the mobile platforms and varying environmental conditions within the subregions, while minimizing the time needed to search each of the subregions. The system and method updates the map of the subregions as needed, in real time, to account for changing environmental conditions and changes in the capabilities of the mobile platforms being used. The subregions may also be determined using a desired level of probability for detecting targets within the subregions in a desired number of passes through the subregion. The system optimizes coverage time while insuring a desired probability of coverage (i.e., observability) for heterogeneous mobile platforms.