One significant coupling problem in missile experience is that which results from interaction between pitch, yaw and roll modes of motion; geometric, aerodynamic and control system couplings and their mutual interactions which give rise to overall system stability problems are considered; supersonic aerodynamic static stability and control characteristics of configuration which experiences aerodynamic coupling in attitude and in control are discussed; functional block diagram of missile steering and roll control system.
Pitch-yaw-roll coupling
AGARD -- Report
1961
15 pages
Report
English
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