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Automatic pilot (Airplanes)
Airplanes 29
Control systems 20
Stability of airplanes 12
Automatic control 10
Flight control 10
Aeronautics 6
Servomechanisms 6
Control 5
Frequency response (Dynamics) 5
Guidance systems (Flight) 5
Mathematical models 5
Yawing (Aerodynamics) 5
Atmospheric turbulence 4
Drone aircraft 4
Guided missiles 4
Aerospace engineering 3
Control theory 3
Flight testing 3
Neural computers 3
Nonlinear systems 3
Robotics 3
Rolling (Aerodynamics) 3
Stability of airplanes, Lateral 3
Aerodynamics, Supersonic 2
Air traffic control 2
Analog computer simulation 2
Automation 2
Electronic differential analyzers 2
Equations of motion 2

A method for predicting the stability in roll of automatically controlled aircraft based on the experimental determination of the characteristics of an automatic pilot / by Jones, Robert T. (Robert Thomas), 1910-1999

Control of autonomous aerial vehicles : advances in autopilot design for civilian UAVs /

An investigation of the stability of a system composed of a subsonic canard airframe and a canted-axis gyroscope automatic pilot / by Gardiner, Robert A.

Effect of an autopilot sensitive to yawing velocty on the lateral stability of a typical high-speed airplane / by Gates, Ordway B.

Bench-test investigation of the transient-response characteristics of several simulated airplanes incorporating an autopilot sensitive to yawing accelerations / by Howard, Donald A.

A survey of stability analysis techniques for automatically controlled aircraft / by Jones, A. L. (Arthur Leslie)

Practical methods of calculation involved in the experimental study of an autopilot and the autopilot-aircraft combination / by Smaus, Louis H.

Theoretical investigation of a proportional-plus-flicker automatic pilot / by Seaberg, Ernest C.

Theoretical investigation of the longitudinal response characteristics of a swept-wing fighter airplane having a pitch-attitude control system / by Stokes, Fred H.

Analogue-computer simulation of an autopilot servo system having nonlinear response characteristics / by Jones, A. L. (Arthur Leslie)

Optimal control theory with aerospace applications / by Ben-Asher, Joseph Z., 1955-

Coping with computers in the cockpit

Analytical study of modification to the autopilot of a fighter airplane in order to reduce the response to side gusts / by Mathews, Charles W.

Theoretical study of the lateral frequency response to gusts of a fighter airplane, both with controls fixed and with several types of autopilots / by Adams, James J.

Laboratory investigation of an autopilot utilizing a mechanical linkage with a dead spot to obtain an effective rate signal / by Seaberg, Ernest C.

A theoretical method of determining the control gearing and time lag necessary for a specified damping of an aircraft equipped with a constant-time-lag autopilot / by Gates, Ordway B.

Automatic control of aircraft and missiles / by Blakelock, John H.

Aviation automation the search for a human-centered approach / by Billings, C. E. (Charles E.), 1929-

Automatic stabilization / by Haus, Fr

Analogue-computer simulation of an autopilot servo system having nonlinear response characteristics / by Jones, Arthur L., White, John S.

Search Results

A method for predicting the stability in roll of automatically controlled aircraft based on the experimental determination of the characteristics of an automatic pilot / by Jones, Robert T. (Robert Thomas), 1910-1999

Control of autonomous aerial vehicles : advances in autopilot design for civilian UAVs /

An investigation of the stability of a system composed of a subsonic canard airframe and a canted-axis gyroscope automatic pilot / by Gardiner, Robert A.

Effect of an autopilot sensitive to yawing velocty on the lateral stability of a typical high-speed airplane / by Gates, Ordway B.

Bench-test investigation of the transient-response characteristics of several simulated airplanes incorporating an autopilot sensitive to yawing accelerations / by Howard, Donald A.

A survey of stability analysis techniques for automatically controlled aircraft / by Jones, A. L. (Arthur Leslie)

Practical methods of calculation involved in the experimental study of an autopilot and the autopilot-aircraft combination / by Smaus, Louis H.

Theoretical investigation of a proportional-plus-flicker automatic pilot / by Seaberg, Ernest C.

Theoretical investigation of the longitudinal response characteristics of a swept-wing fighter airplane having a pitch-attitude control system / by Stokes, Fred H.

Analogue-computer simulation of an autopilot servo system having nonlinear response characteristics / by Jones, A. L. (Arthur Leslie)

Optimal control theory with aerospace applications / by Ben-Asher, Joseph Z., 1955-

Coping with computers in the cockpit

Analytical study of modification to the autopilot of a fighter airplane in order to reduce the response to side gusts / by Mathews, Charles W.

Theoretical study of the lateral frequency response to gusts of a fighter airplane, both with controls fixed and with several types of autopilots / by Adams, James J.

Laboratory investigation of an autopilot utilizing a mechanical linkage with a dead spot to obtain an effective rate signal / by Seaberg, Ernest C.

A theoretical method of determining the control gearing and time lag necessary for a specified damping of an aircraft equipped with a constant-time-lag autopilot / by Gates, Ordway B.

Automatic control of aircraft and missiles / by Blakelock, John H.

Aviation automation the search for a human-centered approach / by Billings, C. E. (Charles E.), 1929-

Automatic stabilization / by Haus, Fr

Analogue-computer simulation of an autopilot servo system having nonlinear response characteristics / by Jones, Arthur L., White, John S.

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