Configuration Design of a Helicopter Integrated Navigation System

Authors
  1. Fingerote, S.I.
  2. Reid, D.B.
  3. Liang, D.F.
  4. Vallot, L.
  5. Greene, C.
  6. Mahesh, J.
Corporate Authors
Honeywell Ltd, Markham ONT (CAN) Advanced Technology Centre;Defence Research Establishment Ottawa, Ottawa ONT (CAN);Honeywell Inc, Minneapolis MN (US) Systems and Research Center
Abstract
Results are presented from configuration performance study phase of the Helicopter Integrated Navigation System project sponsored by the Canadian Department of National Defence. A configuration assessment is presented including processor selection, and a discussion of system architecture and configuration tradeoffs leading to a recommended configuration. Results of the system error analysis and the Kalman filter design are presented demonstrating integrated system performance.
Report Number
AGARD-CP-411-PAP-25 — @Paper presented at the Guidance and Control Panel 43rd Symposium held in London, UK, 7-10 October 1986; CONTAINED IN 88-00492
Date of publication
15 Jul 1987
Number of Pages
9
DSTKIM No
88-00486
CANDIS No
53728
Format(s):
Hardcopy

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