Research on the Dynamic Test of Missile′s Altitude Channel
Zhao Bing
Abstract
Zhao Bing
Abstract
In order to test the whole performance of missile-borne radio altimeter,the theoretical and testing principle of the autopilot is analyzed, and the dynamic testing method is proposed, a programmable difference frequency signal generator has been developed to simulate the flying height of missile and make the auto-tester possessing the ability of dynamic test for altitude channel of missile, it′s also used in the emulation of whole missile trajectory.
A significance statement is not available in the OpenAlex record.
A contribution statement is not available in the OpenAlex record.
Method details are not available in the OpenAlex metadata.
Findings are not separately available in the OpenAlex metadata.
Limitations are not available in the OpenAlex metadata.
Application details are not available in the OpenAlex metadata.
In order to test the whole performance of missile-borne radio altimeter,the theoretical and testing principle of the autopilot is analyzed, and the dynamic testing method is proposed, a programmable difference frequency signal generator has been developed to simulate the flying height of missile and make the auto-tester possessing the ability of dynamic test for altitude channel of missile, it′s also used in the emulation of whole missile trajectory.
Key concepts: Missile, Emulation, Autopilot, Engineering, Missile guidance, Trajectory, Cruise missile, Aerospace engineering