History of Low-Order Equivalent Systems for Aircraft Flying Qualities
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[1] John Hodgkinson,et al. V/STOL Equivalent Systems Analysis. , 1980 .
[2] Eric Potsdam,et al. An analysis of feel system effects on lateral flying qualities , 1990 .
[3] A Morelli Eugene,et al. Low Order Equivalent System Identification for the Tu-144LL Supersonic Transport Aircraft , 2000 .
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[5] Randall Bailey,et al. Initial results of an in-flight investigation of longitudinal flyingqualities for augmented, large transports in approach and landing , 1993 .
[6] Rogers E Smith. Effects of Control System Dynamics on Fighter Approach and Landing Longitudinal Flying Qualities. (Volume I). , 1978 .
[7] A Morelli Eugene. Identification of Low Order Equivalent System Models From Flight Test Data , 2000 .
[8] J. Hodgkinson,et al. The Use and Effectiveness of Piloted Simulation in Transport Aircraft Research and Development , 1992 .
[9] David J. Moorhouse,et al. The control system design methodology of the STOL and Manoeuvre Technology Demonstrator , 1994 .
[10] Randall E. Bailey,et al. Interaction of feel system and flight control system dynamics on lateral flying qualities , 1988 .
[11] M. Marchand,et al. EFA Flying Qualities Specification and its Utilisation. , 1993 .
[12] D. E. Bischoff,et al. Development of Lateral-Directional Equivalent System Models for Selected U.S. Navy Tactical Aircraft. , 1983 .
[13] Di Franco,et al. IN-FLIGHT INVESTIGATION OF THE EFFECTS OF HIGHER-ORDER CONTROL SYSTEM DYNAMICS ON LONGITUDINAL HANDLING QUALITIES , 1968 .
[14] J. M. Stifel. A Time Response Approach to Equivalent Aircraft Dynamics , 1979 .
[15] J. Hodgkinson,et al. Initial results of an inflight simulation of augmented dynamics in fighter approach and landing , 1979 .
[16] Eugene A. Morelli,et al. Low order equivalent system identification for the Tu-144LL supersonic transport aircraft , 2000 .
[17] Wim de Boer,et al. Flight Control Design - Best Practices , 2000 .
[18] Jay M. Brandon,et al. Ground-to-Flight Handling Qualities Comparisons for a High Performance Airplane , 1995 .
[19] David G. Mitchell,et al. Low-Order Approaches to High-Order Systems: Problems and Promises , 1982 .
[20] William S. Levine,et al. CONDUIT: A New Multidisciplinary Integration Environment for Flight Control Development , 1997 .
[21] David E Bischoff. Development of Longitudinal Equivalent System Models for Selected U.S. Navy Tactical Aircraft , 1981 .
[22] Roger H. Hoh,et al. Development of Handling Quality Criteria for Aircraft with Independent Control of Six Degrees of Freedom , 1981 .
[23] Rogers E. Smith,et al. An In-Flight Investigation to Develop Control System Design Criteria for Fighter Airplanes. Volume 1 , 1970 .
[24] S. K. Sarrafian,et al. Effect of time delay on flying qualities - An update , 1986 .
[25] M. F. Shafer. Low order equivalent models of highly augmented aircraft determined from flight data using maximum likelihood estimation , 1980 .
[26] Samuel J. Craig,et al. An Analysis of Navy Approach Power Compensator Problems and Requirements. , 1971 .
[27] R. J. Wilson,et al. In-Flight Evaluation of Control System Pure Time Delays , 1982 .
[28] D E Bischoff. The Control Anticipation Parameter for Augmented Aircraft. , 1981 .
[30] John Hodgkinson,et al. Aircraft Handling Qualities , 1999 .
[31] J. Hodgkinson,et al. Interpreting the handling qualities of aircraft with stability and control augmentation , 1990 .
[32] J. Hodgkinson,et al. Equivalent system approaches to handling qualities analysis and design problems of augmented aircraft , 1977 .
[33] R. C. Radford,et al. Landing flying qualities evaluation criteria for augmented aircraft , 1980 .
[34] J. Hodgkinson,et al. Handling qualities of aircraft with stabilty and control augmentation systems—a fundamental approach , 1976, The Aeronautical Journal (1968).
[35] R. Hoh,et al. An alternate method of specifying bandwidth for flying qualities , 1982 .
[36] John Hodgkinson,et al. Longitudinal and lateral-directional flying qualities investigation of high-order characteristics for advanced-technology transports , 1993 .
[37] T. Gentry. Guidance for the use of equivalent systems with MIL-F-8785C , 1982 .
[38] David G. Mitchell,et al. Determining bandwidth in the presence of nonlinearities , 1999 .
[39] Charles R. Chalk,et al. Background Information and User Guide for Mil-F-8785B (ASG), 'Military Specification-Flying Qualities of Piloted Airplanes' , 1969 .
[40] David G. Mitchell,et al. Proposed MIL Standard and Handbook - Flying Qualities of Air Vehicles. Volume 2. Proposed MIL Handbook , 1982 .