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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1986, Vol. 7 ›› Issue (4): 393-398.

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THE APPLICATION OF ALTITUDE OBSERVATION IN CNI RELATIVE NAVIGATION

Wang Dun, Ding Ziming   

  1. Beijing Institute of Aeronautics and Astronautics
  • Received:1985-04-16 Revised:1900-01-01 Online:1986-09-25 Published:1986-09-25

Abstract: Results of computer simulation show that, communication, navigation and identification (CNI) integerated system has larger estimation error in altitude if there is not any other observation. The error can be reduced by using altitude observation. In practice the Kalman filter can be decoupled on the basis of distribution of members of CNI system.