Abstract: A computer system has processing circuitry to manage a vehicle having an Automated Driving System (ADS). The ADS is configured to control the motion of the vehicle when the vehicle is configured in an autonomous mode. The processing circuitry is configured to estimate State of Health (SoH) of one or more control systems of the vehicle. The one or more control systems are configured to control the use of the autonomous mode. The processing circuitry is configured to, based on the estimated SoH, determine whether or not the vehicle shall use the autonomous mode.

Abstract: A computer system comprising processing circuitry configured to: receive a first vehicle operation command defining a first desired operation of an autonomous vehicle; control a primary vehicle system to perform the first desired operation; send a request for testing a secondary vehicle system being a backup of the primary vehicle system; receive an indication that a present traffic situation is suitable for testing the secondary vehicle system; receive a second vehicle operation command defining a second desired operation of the autonomous vehicle; control the secondary vehicle system to perform the second desired operation; receive a third vehicle operation command defining a third desired operation of the autonomous vehicle; and control the primary vehicle system to perform the third desired operation.

Abstract: The invention relates to a method for control of a flying wing. The flying wing is arranged to be controlled to move along a predetermined trajectory by means of a fluid stream passing a wing of the flying wing. The flying wing comprises at least one control surface for controlling the movement of the flying wing along the predetermined trajectory. The flying wing is positioned in a reference frame where the x-axis is directed horizontally along a level L above which the flying wing moves, the y-axis is perpendicular to the x-axis in a vertical direction and the z-axis is perpendicular to the x-axis along the level L in a direction along the principal direction of the fluid stream. The invention further relates to a system comprising a flying wing and a computer-readable medium for use with a flying wing.

Abstract: The invention relates to a method for control of a flying wing. The flying wing is arranged to be controlled to move along a predetermined trajectory by means of a fluid stream passing a wing of the flying wing. The flying wing comprises at least one control surface for controlling the movement of the flying wing along the predetermined trajectory. The flying wing is positioned in a reference frame where the x-axis is directed horizontally along a level L above which the flying wing moves, the y-axis is perpendicular to the x-axis in a vertical direction and the z-axis is perpendicular to the x-axis along the level L in a direction along the principal direction of the fluid stream. The invention further relates to a system comprising a flying wing and a computer-readable medium for use with a flying wing.