Abstract: The display of images, such as panoramic images, in a limited display space can be aided through the use of motion-based control, whereby a user can rotate and/or translate a computing device in order to view different portions of the image, including translating or zooming within the image. Sensors can be used to determine the motion for adjusting the display. The same or other sensors can also assist a user in capturing such an image. For example, a compass can determine the relative orientation of the device and a gyroscope can determine rotation of the device, to determine an appropriate path of motion for the capture and any deviation from that path. The user can be provided with information enabling the user to follow the path with an appropriate device orientation.

Abstract: The display of images, such as panoramic images, in a limited display space can be aided through the use of motion-based control, whereby a user can rotate and/or translate a computing device in order to view different portions of the image, including translating or zooming within the image. Sensors can be used to determine the motion for adjusting the display. The same or other sensors can also assist a user in capturing such an image. For example, a compass can determine the relative orientation of the device and a gyroscope can determine rotation of the device, to determine an appropriate path of motion for the capture and any deviation from that path. The user can be provided with information enabling the user to follow the path with an appropriate device orientation.

Abstract: A UAV includes: a rocket body, having a rocket motor and a payload section; a parachute coupled with the payload section; an image capture device; a magnetometer to provide a compass reference for images taken from the image capture device; and a transmitter to communicate image and compass data to a remote receiver. Compass bearings are overlaid on image data from the image capture device. A handheld launch unit includes an ignition system, having an activation mechanism and an igniter to activate the rocket motor. A safety pin prevents electrical current from flowing to the igniter until the pin is removed. An accelerometer and/or magnetometer determines an angular orientation of the UAV. Software verifies that the angle is within a user-defined safety limit before activating the igniter.