A method for providing medical services to a patient, including: receiving a medical service request associated with a patient location; selecting an aircraft, located at an initial location, from a plurality of aircraft based on the patient location and the initial location; determining a flight plan for flying the aircraft to a region containing the patient location; at a sensor of the aircraft, sampling a first set of flight data; at a processor of the aircraft, autonomously controlling the aircraft to fly based on the flight plan and the set of flight data; selecting a landing location within the region; and landing the aircraft at the landing location, including: sampling a set of landing location data; determining a safety status of the landing location based on the set of landing location data; outputting a landing warning observable at the landing location; at the sensor, sampling a second set of flight data; and in response to determining the safety status and outputting the landing warning, autonomously controlling the aircraft to land at the landing location based on the second set of flight data.

A method for providing medical services to a patient, including: receiving a medical service request associated with a patient location; selecting an aircraft, located at an initial location, from a plurality of aircraft based on the patient location and the initial location; determining a flight plan for flying the aircraft to a region containing the patient location; at a sensor of the aircraft, sampling a first set of flight data; at a processor of the aircraft, autonomously controlling the aircraft to fly based on the flight plan and the set of flight data; selecting a landing location within the region; and landing the aircraft at the landing location, including: sampling a set of landing location data; determining a safety status of the landing location based on the set of landing location data; outputting a landing warning observable at the landing location; at the sensor, sampling a second set of flight data; and in response to determining the safety status and outputting the landing warning, autonomously controlling the aircraft to land at the landing location based on the second set of flight data.

A solar power panel failure search and detect system to search and detect malfunctioning or failed sites of a solar power panel. A search unit is installed in a remotely controllable aerial vehicle. The search unit maintains a constant distance between a solar panel and a failure detector, and maintains the failure detector at an optimum angle. A control unit controls a flight path and a flight angle of the aerial vehicle and controls/regulates an angle of the failure detector, a receiver, a processor, and the search unit. The search unit has an angle sensor, the failure detector, an angle adjuster and an imaging device. The control unit has a transmitter to transmit the search result data.

Methods and apparatus for positioning aircraft based on images of mobile targets are disclosed. An example method includes identifying, by executing first instructions via a processor, a mobile target in an image obtained by a camera mounted on a first aircraft and obtaining, by executing second instructions via the processor, current coordinates of the first aircraft. The example method includes determining, by executing third instructions via the processor, coordinates of the mobile target based on the coordinates of the first aircraft and the image. The coordinates of the mobile target are within an area of uncertainty. The example method includes determining, by executing fourth instructions via the processor, a first position for the first aircraft that reduces the area of uncertainty of the coordinates of the mobile target.

A package enclosure for use on an aerial vehicle including an outer skin having left and right side walls and a front end and a rear end, a base positioned within the outer skin exerting a force against inner surfaces of the left and right side walls of the outer skin, and a handle upwardly extending from the base.

The systems and methods are provided to provide communication coverage to an unmanned aerial vehicle. A proposed flight path of a UAV may be collected, and a communication signal distribution, such as a cellular signal distribution, along the proposed flight of the UAV may be determined. At positions having low or no communication signal, relays may be provided to improve a quality of the communication signal. The relay may be a ground device or an aerial vehicle. A stable and continuous communication between the UAV and user terminals during the entire flight path of UAV may be provided, and a coverage of cellular signal may be expanded.

A system for controlling weight distribution of a remotely piloted aircraft is described. The system comprises a payload weighing platform, a control unit, and a counterweight gantry system. The payload weighing platform is configured to be positioned within the aircraft and receive the payload. The control unit is configured to: receive payload sensor data from the payload weighing platform; determine payload weight and payload center of mass; determine a target position for each of at least one counterweight, the target position determined to control a center of gravity of the aircraft by controlling the weight distribution of the aircraft; and provide a counterweight position signal to the counterweight gantry system. The counterweight gantry system is attached to the aircraft and is configured to move each of the at least one counterweight to corresponding target position in response to receiving the counterweight position signal.

Techniques are described for configuring a monitoring system to assist users during a detected emergency condition at a property. In some implementations, sensor data from one or more sensors that are located at the property are obtained by a monitoring system that is configured to monitor the property. A determination that there is an emergency condition at the property is made by the monitoring system based on the sensor data, determining. A location of a person inside the property is determined by the monitoring system based on the sensor data. A first path to the person and a second path to guide the person away from the emergency condition are determined by the monitoring system. The first path to the person and the second path to guide the person away from the emergency condition are navigated by a computing device of the monitoring system.

An aircraft with an airframe and at least one thrust producing unit the at least one thrust producing unit being electrically powered by an associated electrical engine that is electrically connected to an electrical energy source via an electrical energy distribution system, wherein the airframe comprises at least one load carrying section and at least one propulsion system carrying section, wherein the at least one load carrying section and the at least one propulsion system carrying section are segregated from each other, wherein the at least one load carrying section is provided for transportation of passengers and/or cargo, and wherein the at least one propulsion system carrying section is provided for carrying at least essentially the electrical energy source and the electrical energy distribution system.

Techniques are described for configuring a monitoring system to assist users during a detected emergency condition at a property. In some implementations, sensor data from one or more sensors that are located at the property are obtained by a monitoring system that is configured to monitor the property. A determination that there is an emergency condition at the property is made by the monitoring system based on the sensor data, determining. A location of a person inside the property is determined by the monitoring system based on the sensor data. A first path to the person and a second path to guide the person away from the emergency condition are determined by the monitoring system. The first path to the person and the second path to guide the person away from the emergency condition are navigated by a computing device of the monitoring system.