초록 ▼

A stationary test device for a missile includes a retaining device for an avionics testpiece of the missile, where the retaining device enables a movement of the avionics testpiece in three rotational degrees of freedom, and a display device configured to display information on the missile surroundi

A stationary test device for a missile includes a retaining device for an avionics testpiece of the missile, where the retaining device enables a movement of the avionics testpiece in three rotational degrees of freedom, and a display device configured to display information on the missile surroundings, where the display device is configured to be moved inside a virtual plane by a translational carriage system. The display device can be detected by the avionics testpiece if the avionics testpiece is disposed on the retaining device. A mobile test device for the missile includes a flight platform, a carrier device mounted on the flight platform, for an avionics testpiece of the missile, wherein the carrier device enables a movement of the avionics testpiece in three rotational degrees of freedom, and a control module, where the control module is configured to control the flight platform for taking off on a specified reference trajectory, control the carrier device for orientation of the avionics testpiece, and store navigation data generated by the avionics testpiece. Finally, a test system for the missile includes the stationary test device and the mobile test device.

대표청구항 ▼

1. A test system for a missile comprising: a mobile test device comprising: a flight platform;a carrier mounted on the flight platform, for an avionics testpiece of the missile, wherein the carrier enables a movement of the avionics testpiece in three rotational degrees of freedom; anda control modu

1. A test system for a missile comprising: a mobile test device comprising: a flight platform;a carrier mounted on the flight platform, for an avionics testpiece of the missile, wherein the carrier enables a movement of the avionics testpiece in three rotational degrees of freedom; anda control module configured to:control the flight platform for taking off on a specified reference trajectory,control the carrier for orientation of the avionics testpiece, andstore navigation data generated by the avionics testpiece; anda stationary test device for a missile comprising: a retainer for an avionics testpiece of the missile, wherein the retainer enables a movement of the avionics testpiece in three rotational degrees of freedom, anda display configured to display information on surroundings of the avionics testpiece, wherein the display is configured to be moved in a plane by a translational carriage system,wherein the display can be detected by the avionics testpiece when the avionics testpiece is disposed on the retainer,wherein the stationary test device further comprises a control unit by which a movement of the retainer and a movement of the display is controllable in order to simulate taking off on a pre-defined reference trajectory, and by which navigation data generated by the avionics testpiece can be stored, andwherein the stationary test device is operable with simulation data obtained from measurement data captured during the operation of the mobile test device. 2. The test system according to claim 1, wherein the retainer of the stationary test devices is a turntable or a robot. 3. The test system according to claim 1, wherein the simulation data obtained from the measurement data obtained during the operation of the mobile test device comprise Inertial Measurement Unit data, Global Positioning System data, Control Actuator System data and seeker head data. 4. The test system according to claim 1, wherein the carrier comprises a gimbal platform. 5. The test system according to claim 1, wherein the flight platform comprises a helicopter with at least two horizontally oriented rotors. 6. A method for testing missiles with a test system for a missile, the test system comprising: a mobile test device comprising: a flight platform;a carrier mounted on the flight platform, for an avionics testpiece of the missile, wherein the carrier enables a movement of the avionics testpiece in three rotational degrees of freedom; anda control module configured to:control the flight platform for taking off on a specified reference trajectory,control the carrier for orientation of the avionics testpiece, andstore navigation data generated by the avionics testpiece; anda stationary test device for a missile comprising: a retainer for an avionics testpiece of the missile, wherein the retainer enables a movement of the avionics testpiece in three rotational degrees of freedom, anda display configured to display information on the surroundings of the avionics testpiece, wherein the display is configured to be moved in a plane by a translational carriage system,wherein the display can be detected by the avionics testpiece when the avionics testpiece is disposed on the retainer,wherein the stationary test device further comprises a control unit by which a movement of the retainer and a movement of the display is controllable in order to simulate taking off on a pre-defined reference trajectory, and by which navigation data generated by the avionics testpiece can be stored, andwherein the stationary test device is operable with simulation data obtained from measurement data captured during the operation of the mobile test device,the method comprising:defining a reference trajectory which is translational and simulates a relative geometry between a missile and a target of the missile;taking off on the reference trajectory using the mobile test device, wherein an avionics testpiece of the missile is disposed on the mobile test device; andsimulating a movement of the missile based on simulation data with the stationary test device, wherein the avionics testpiece is disposed on the stationary test device and wherein the simulation data are based on the measurement data obtained during said taking off on the reference trajectory.