Pseudo-range/pseudo-range rate tight integration method for inertial/satellite navigation system
Patent Information
- Authority / Receiving Office
- CN · China
- Current Assignee / Owner
- BEIJING AUTOMATION CONTROL EQUIP INST
- Publication Date
- 2013-03-27
- Estimated Expiration
- Not applicable · inactive patent
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Abstract
Description
technical field
[0001] The invention belongs to the technical field of inertial / satellite integrated navigation, in particular to an inertial / satellite navigation system pseudo-range / pseudo-range rate tight combination method. Background technique
[0002] The inertial / satellite integrated navigation system has penetrated into the military and aerospace fields, and plays an important role in maintaining national security and promoting economic growth.
[0003] Since the satellite navigation system is easily affected by the interference of the electromagnetic environment, complex terrain, trees, and buildings, the number of visible satellites is reduced, and it cannot be positioned normally, so that the inertial / satellite integrated navigation system is used in navigation such as electronic warfare battlefields, valleys, and riverbeds, oil and gas The use in complex environments such as surveying and blind guide services between urban buildings is greatly restricted. The trad...