Method for the determination of inertial measured variables
DE102011115963B3
Unmanned training and test missile
DE102011114225B3
Missile training unit for use in aircraft, has configuration unit connected to missile, and flight body-hardware remaining unchanged, where missile is actually presented as simulated error that is stored in error storage unit
DE102011109693B3
Structure component for an operational missile system
DE102011108077A1
Method of memory management in a multitasking data processing system
DE102011107630A1
Steer a vehicle towards a destination
DE102011018947A1
Firearm aiming device and firearm, and method for aligning a firearm
DE102011015780A1
Small aircraft
DE102011010987A1
Navigation method for a missile
DE102011009872A1
Method and device for modulating the clamping voltages of a three-phase synchronous motor with non-sinusoidal electromotive characteristic and three-phase three-phase motor
DE102010053896A1
Target engagement system
DE102010027189A1
Seeker head for a missile
DE102010026452A1
Method for data transmission between a base station and a missile and missile for carrying out this method
DE102010019936A1
Method for qualifying e.g. combat aircraft, involves determining qualification value of object under consideration of detected property value, where qualification values for two classes of classification are not equal to zero
DE102010019147A1
Method and device for tracking the trajectory of a moving object and computer program and data carrier
DE102010018143A1
Method for determining position data of a target object in a reference system
DE102010018144A1
Method for automatically generating a three-dimensional reference model as terrain information for an imaging device
DE102010017974A1
A method of simulating an unmanned armed missile mission
DE102010011263A1
Apparatus and method for determining the position and / or speed of a device in a satellite navigation system