It Is logical to conclude however, that Mp, gain margin, and phase margin criteria give reasonable answers about the transient response In ... a#39;Theory of Servomechanisuis, a#39; by Janes, Nichols, and Phillips, McQraw Hill Book Co., 1947. ... a#39;Analysis of Feedback Systems by the Open Loop Closed Loop Logarithmic Method, a#39; by D. T. McRuer and R. Zacharlas, Northrop Aircraft, Inc., Unpublished paper, 1952.
|Title||:||Bureau of Aeronautics Flight Control System Manuals: Methods of analysis and synthesis of piloted aircraft flight control systems|
|Author||:||Northrop Corporation. NORAIR Division|