Results 11 to 20 of about 8,660 (228)
Autopilot Structured H∞ Synthesis for Satisfying Gain and Phase Margin Constraints [PDF]
Aiming at the static unstable Hypersonic vehicle, a method for designing H∞ autopilot to satisfy gain margin and phase margin is proposed. Structured H∞ synthesis is used to synthesize the autopilot under the fixed structure.
doaj +2 more sources
Robust autopilot of the pitch channel of unmanned aircraft vehicles [PDF]
Automatic pitch control system of unmanned aircraft vehicles (UAVs) with different aerodynamic configuration and airframe construction is reflected here. Robust autopilot scheme is proposed for such control system. While adjusting the parameters of UAV’s
Yu. V. Gridnev, A. G. Ivanov
doaj +2 more sources
PX4/PX4-Autopilot: v1.14.0-rc1 [PDF]
<p>Release Candidate v1.14.0</p> What's Changed <ul> <li>[New] Dynamic Control Allocation</li> <li>[New] Default simulation is now New Gazebo</li> <li>[New] Improved ROS 2 Interface thanks to uXRCE-DDS< ...
Silvan Fuhrer +29 more
core +1 more source
A hardware implementation of 6dof quadcopter matlab/simulink controller algorithm to an autopilot [PDF]
This paper presents a hardware implementation of Control algorithm for 6DOF Quadcopter developed on MATLAB/SIMULINK to an autopilot Microcontroller (PIXHAWK) using MATLAB/SIMULINK Embedded Coder.
Amar, Bousbaine +2 more
core +2 more sources
A Novel Design and Implementation of an Autopilot Terrain-Following Airship
Unmanned Aerial vehicles (UAV) have been utilized in many application domains. UAVs (or Airships, e.g., Drones) have been adopted to explore resources (e.g., minerals). One of the main limitations of using such airships is that flying at a fixed altitude
Seulki Lee +3 more
doaj +1 more source
Non-linear autopilot design using the philosophy of variable transient response [PDF]
The novel non-linear controller design methodology of Variable Transient Response (VTR) is presented in this research. The performance of VTR is compared to that of successful non-linear controller designs (such as Robust Inverse Dynamics Estimation and ...
Macdonald, Malcolm +6 more
core +1 more source
Consistent Design of PID Controllers for an Autopilot
A consistent approach to the development of tuning rules for course-keeping and path-tracking PID controllers for a ship autopilot are presented. The consistency comes from the observation that for each of the controllers the controlled plant can be ...
Świder Zbigniew +2 more
doaj +1 more source
Coupled 6DoF nonlinear model of tactical missiles: an optimal autopilot design [PDF]
A fully coupled six degrees of freedom modelling of a tactical missile and an optimal control theory-based method are presented aiming at minimizing the autopilot control effort and improving the accuracy of reaching the target by a missile guidance ...
Tadeusz Mikutel +2 more
doaj +1 more source
Nonlinear Three-Loop Autopilot Design for Spaceplanes [PDF]
This paper deals with the nonlinear autopilot design for spaceplanes based on the three-loop autopilot architecture. To this end, the nonlinear dynamics equations for spaceplanes during the reentry phase are first determined.
Yoon, Dain +3 more
core +1 more source
Robust Adaptive Output Feedback Control for a Guided Spinning Rocket
An adaptive autopilot is presented for the pitch and yaw channels of a guided spinning rocket. Firstly, the uncertain dynamic model of a guided spinning rocket is established, which is used to evaluate the performance of the proposed adaptive autopilot ...
Zhongjiao Shi, Liangyu Zhao, Yeqing Zhu
doaj +1 more source

