Automatic stability control device for aircraftdoi:US2985410 ARalph R HeppeCelniker LeoHeinz K RichterUSUS2985410 * Mar 27, 1957 May 23, 1961 Lockheed Aircraft Corp Automatic stability control device for aircraft
Fundamentally we have to discern between the stability of the aircraft to external impetus, with and without the pilot responding to the perturbation. Here we will limit ourselves to the inherent stability of the aircraft. Hence the aircraft is said to be stable if it returns back to its origi...
The performance, stability, control and response of aircraft are key areas of aeronautical engineering. This book provides a comprehensive overview to the underlying theory and application of what are often perceived to be difficult topics. Initially it introduces the reader to the fundamental concepts...
Flight path stability augmentation 7. Improved flight handling qualities 8. Flight data recording 9. Collision avoidance 10. Formation flying (military) 11. Target acquisition (military) 12. Secure identification (military) 13. Crew/passengers comfort improvement 14. Structural load alleviation 15. Terr...
Then the stability of the overall system is analyzed and global control is introduced to compensate coupling among some of the subsystems. In the book a particular choice of subsystems is proposed in a case of flight control, and the local and global control synthesis is presented. Extensive ...
F. G. Garashchenko and N. F. Kirichenko, “Studying problems of practical stability and motion stabilization, ” Mekh. Tverd. Tela, No. 6, 15–24 (1975). V. M. Kuntsevich and M. M. Lychak, Lyapunov-Function Synthesis of Automatic Control Systems [in Russian], Nauka, Kiev (1977)...
Stability derivatives; Helicopter; Angle of attack; Vertical stabilizer; Actuator; Attitude control; Root locus; Flight envelope; Autocorrelation; Wing configuration; Phugoid; Airfoil; Jet engine; Airborne early warning and control; Fixed-wing aircraft; Cruise (aeronautics); Right half-plane; Helicopter...
10. Inputs and System Performance Assessment 537 11. Multiloop Flight Control Systems 600 APPENDICES A. Stability Derivatives and Transfer Function Factors for Representative Aircraft 687 APPENDICES B. Elements of Probability 744 Supplementary Bibliography for Aircraft Dynamics and Automatic Control 769...
2838255 Automatic emergency radio control system 1958-06-10 2768343 Angular velocity control device for aircraft 1956-10-23 2767942 Apparatus limiting acceleration forces on aircraft 1956-10-23 2761998 Pulse lengthening circuit 1956-09-04 2701111 Cruise control apparatus 1955-02-01 2630284 Stick...
Automatic stability control device United States Patent 3116042 Inventors: Richter, Heinz K. Heppe, Ralph R. Leo, Celniker Application Number: US5625860A Publication Date: 12/31/1963 Filing Date: 09/15/1960 Export Citation: Click for automatic bibliography generation...