Development of Attitude Constraints for Real-time Attitude Determination System using GPS carrier phase

摘要: As one of validation tool for attitude determination system, we have used various constraints using priori information which is known through base vector set up. However these conventional cannot guarantee validity in terms final solutions such as Euler angle. So suggest boundary concept to verify the solution on flying airplane, it based combination velocity estimation technique and ambiguity resolution. can say check invalid effectively at just epoch without repeatability test resolved cycle ambiguity. In this paper show that suggested constraint reject incorrectly missed.