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Fundamentals of Design of Piloted Aircraft Flight Control Systems - Vol II, Addendum 1 - Dynamics of the Airframe

The material of this addendum forms part of Report AE-61-G) which together with 
Report AE-61-41, has been written under BuAer Contract Nus 51-514(c), "Amda- 
mentali of Aircraft Flight Control $stems. " These form part of a 
series of manuals being written for the purpose of providing a unified approach to 
problems of control system design. 
For the sake of securing-as vide a as possible, Report AE-6i-41, "Meth- 
ods of Analysis and Synthesis, which Is Volume I of this series, and the part, "Dy- 
namics of the Airframe" (Vol. L), of AE-61-411 which precedes this confidential 
addenå•m, have been issued in an unclassified status. in accordance with one of the 
general intatts of the seriæ to provide a source of information to be used by engineers 
in bridging the gap between their collegiate training and the more advanced topics of 
system engineering. 
Since the figures of this addendum contain classified data, they could not be included 
in the body of this Report, but are presented here in Order to include the maximum 
usable information available at this time. Because of the. disparity in level of classi- 
ficatim, nosmmå0ii of this been -made in tne this Report, but the 
information herein to be considered in conjunction with the contents of Chapter IV.