Method for providing stable, inertially derived altitude indication is described; this method utilizes compensation technique based on inertial acceleration and velocity measurements and using stored density altitude relationships; application to guidance of hypersonic glide vehicles and to use in conjunction with Schuler loops of such vehicles is described, and results of REAC study are presented.
Internal altitude technique for hypersonic glide vehicle guidance
IRE -- East Coast Conference Aerospace Navigational Electronics -- Tech Paper
IRE East Coast Conference on Aerospace and Navigational Electronics ; 1961 Control
1961
8 pages
Aufsatz (Konferenz)
Englisch
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