Flight formation control (23 Ergebnisse)

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Taschenbuch. Zustand: Neu. Neuware - Automating the control of an aircraft flying in formation necessitates the extension of the theory of formation flight control to allow for three dimensional maneuvers. The formation was modeled as a two-aircraft, leader and wingman, formation. Both aircraft has its own three dimensional, rotating and translating, Cartesian axes system, with special attention being given to the motion of the leader in relation to the wingman. The controller operated using the equations of motion expressed in the rotating reference frame of the wing aircraft. The control system has seven states, three inputs and three disturbance signals to model the dynamics of the formation in three dimensional space. The control law employed was the feedback of the difference between in actual separation distance and the commanded separation distance to affect changes in thrust, lift, and roll rate. The control system incorporated proportional, integral, and derivative control elements, each with separate gains, to achieve and maintain the specified formation geometry despite various maneuvers flown by the leader. Simulated maneuvers included: an initial displacement of the wingman away from the formation geometry, and changes in the leader's velocity, altitude, and heading. For each maneuver, the controller performance was sufficient to maintain the commanded formation geometry.…

Taschenbuch. Zustand: Neu. Neuware - The purpose of this research was to further define the position of maximum benefit for the wingman of a two-ship formation of aircraft. An analytical analysis was conducted using a vortex lattice code. Investigations of a similar formation of F-16 aircraft and a dissimilar formation with a KC-135 lead aircraft and F-16 trail aircraft were conducted. The analysis determined the effects of varying airspeed on the optimal position. Additionally, the flight control surface deflections were taken account during the analyses, and the flight control positions were determined to be within the bounds of the F-16 aircraft. The similar formation profile was further investigated during flight test. The flight test investigated the change in vertical positioning as well as lateral spacing from the analytic analysis. The drag savings profile has the capability to increase the range of existing airframes, providing the benefit at no cost.…

Taschenbuch. Zustand: Neu. Neuware - The subject of automatic formation flight control is of current interest to the development of Unmanned Aerial Vehicles (UAV). Previous control approaches have been refined in this work to allow more robust maneuvering and to include a fourth control parameter. The equations of motion for each aircraft as a point mass, expressed in a wind-axis coordinate system, are coupled into differential equations that model the two aircraft system dynamics. Control laws are developed that include proportional and integral action. Gains are determined based on formation performance. Lead maneuvers are simulated and the controller is gauged on its ability to maintain the commanded formations in and out of the vortex wake generated by the lead aircraft. A Dryden wind model at varying intensities is applied to the system. In simulation the controller maintained acceptable performance in all maneuvers tested. A slightly modified controller was applied to a USAF NF-16D aircraft for flight testing. Utilizing a data link system and a virtual lead aircraft generated from a ground based control station, the NF-16D was able to flight test the controller. In-flight, the controller was stable, and able to perform all of the desired formation hold and change maneuvers.This work has been selected by scholars as being culturally important, and is part of the knowledge base of civilization as we know it. This work was reproduced from the original artifact, and remains as true to the original work as possible. Therefore, you will see the original copyright references, library stamps (as most of these works have been housed in our most important libraries around the world), and other notations in the work.This work is in the public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work.As a reproduction of a historical artifact, this work may contain missing or blurred pages, poor pictures, errant marks, etc. Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant. …

Zustand: New. KlappentextrnrnAutomating the control of an aircraft flying in formation necessitates the extension of the theory of formation flight control to allow for three dimensional maneuvers. The formation was modeled as a two-aircraft, leader and wingm.

Zustand: New. KlappentextrnrnThe purpose of this research was to further define the position of maximum benefit for the wingman of a two-ship formation of aircraft. An analytical analysis was conducted using a vortex lattice code. Investigations of a similar .

Taschenbuch. Zustand: Neu. Neuware - A controller is designed for an aircraft to autonomously fly formation during aerial refueling. Requirements for a refueling autopilot are stated. A six-degree-offreedom model is developed for an F-16 lead aircraft and a Learjet LJ-25 wing aircraft. Bare airframe stability of both aircraft is investigated, and stability augmentation is performed. A Matlab Simulink simulation is built to reproduce the sensor inputs that will be available to the wing aircraft in flight, including disturbances. Control frames are investigated to determine the optimum presentation of the error vector for control during the task of air refueling. Control laws are developed from the initial premise of proportional-plus-integral control on position error only, and made more complex until desired performance is achieved. Tanker flight profiles are designed for the lead aircraft, and simulations are accomplished to estimate controller performance. Stability and robustness are investigated through the addition of noise, turbulence, and time delays while exploring the capability limits during increasingly aggressive profiles. Modifications for flight test are described, and flight test results are reviewed from 7 formation flights of a USAF C-12 and a Learjet LJ-25 under fully autonomous control in an operationally representative refueling environment. Actual controller performance is analyzed and compared to predictions, and suggestions are made for future controllers.This work has been selected by scholars as being culturally important, and is part of the knowledge base of civilization as we know it. This work was reproduced from the original artifact, and remains as true to the original work as possible. Therefore, you will see the original copyright references, library stamps (as most of these works have been housed in our most important libraries around the world), and other notations in the work.This work is in the public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work.As a reproduction of a historical artifact, this work may contain missing or blurred pages, poor pictures, errant marks, etc. Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant.…

Zustand: New. KlappentextrnrnThe subject of automatic formation flight control is of current interest to the development of Unmanned Aerial Vehicles (UAV). Previous control approaches have been refined in this work to allow more robust maneuvering and to incl.

Buch. Zustand: Neu. Neuware.

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Zustand: New. In the last decade the development and control of Unmanned Aerial Vehicles (UAVs) has attracted a lot of interest. Both researchers and companies have a growing interest in improving this type of vehicle given their many civilian and military applications. This book presents the state of the art in the area of UAV Flight Formation. Editor(s): Guerrero, Josep; Lozano, Rogelio. Num Pages: 340 pages, Illustrations. BIC Classification: TJFM1; TRP. Category: (G) General (US: Trade). Dimension: 239 x 158 x 24. Weight in Grams: 642. . 2012. . . . .…

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Gebunden. Zustand: New. In the last decade the development and control of Unmanned Aerial Vehicles (UAVs) has attracted a lot of interest. Both researchers and companies have a growing interest in improving this type of vehicle given their many civilian and military applications.T.

Zustand: New. In the last decade the development and control of Unmanned Aerial Vehicles (UAVs) has attracted a lot of interest. Both researchers and companies have a growing interest in improving this type of vehicle given their many civilian and military applications. This book presents the state of the art in the area of UAV Flight Formation. Editor(s): Guerrero, Josep; Lozano, Rogelio. Num Pages: 340 pages, Illustrations. BIC Classification: TJFM1; TRP. Category: (G) General (US: Trade). Dimension: 239 x 158 x 24. Weight in Grams: 642. . 2012. . . . . Books ship from the US and Ireland.…

Buch. Zustand: Neu. Neuware - In the last decade the development and control of Unmanned Aerial Vehicles (UAVs) has attracted a lot of interest. Both researchers and companies have a growing interest in improving this type of vehicle given their many civilian and military applications.This book presents the state of the art in the area of UAV Flight Formation. The coordination and robust consensus approaches are presented in detail as well as formation flight control strategies which are validated in experimental platforms. It aims at helping students and academics alike to better understand what coordination and flight formation control can make possible.Several novel methods are presented:- controllability and observability of multi-agent systems;- robust consensus;- flight formation control;- stability of formations over noisy networks;which generate solutions of guaranteed performance for UAV Flight Formation.Contents1. Introduction, J.A. Guerrero.2. Theoretical Preliminaries, J.A. Guerrero.3. Multiagent Coordination Strategies, J.A. Guerrero, R. Lozano, M.W. Spong, N. Chopra.4. Robust Control Design for Multiagent Systems with Parametric Uncertainty, J.A. Guerrero, G. Romero.5. On Adaptive and Robust Controlled Synchronization of Networked Robotic Systems on Strongly Connected Graphs, Y.-C. Liu, N. Chopra.6. Modeling and Control of Mini UAV, G. Flores Colunga, J.A. Guerrero, J. Escareño, R. Lozano.7. Flight Formation Control Strategies for Mini UAVs, J.A. Guerrero.8. Formation Based on Potential Functions, L. García, A. Dzul.9. Quadrotor Vision-Based Control, J.E. Gomez-Balderas, J.A. Guerrero, S. SALAZAR, R. Lozano, P. Castillo.10. Toward Vision-Based Coordination of Quadrotor Platoons, L.R. García Carrillo, J.A. Guerrero, R. Lozano.11. Optimal Guidance for Rotorcraft Platoon Formation Flying in Wind Fields, J.A. Guerrero, Y. Bestaoui, R. Lozano.12. Impact of Wireless Medium Access Protocol on the Quadrotor Formation Control, J.A. Guerrero, Y. Challal, P. Castillo.13. MAC Protocol for Wireless Communications, A. Mendez, M. Panduro, O. Elizarraras, D. Covarrubias.14. Optimization of a Scannable Pattern for Bidimensional Antenna Arrays to Provide Maximum Performance, A. Reyna, M.A. Panduro, A. Mendez.…

paperback. Zustand: New. Language:Chinese.Spacecraft formation flight dynamics control and navigation.

paperback. Zustand: New. Pub Date: 2014-08-01 Pages: 256 Language: Chinese Publisher: National Defense Industry Press flight formation control. the latest research results mainly with aircraft flying in formation of autonomous research and its application has been made to authors in the field The accumulation of the main line of research are proposed multi-agent coordination strategy with parameter uncertainty multi-agent system robust control design methods. strongly connected graph from the network robot system. ad.…

Hardcover. Zustand: New. HardCover. Pub Date: 2015-09-01 Pages: 224 Language: Chinese Publisher: Science Press docking of spacecraft flying in formation is the electromagnetic current international aerospace research and a new hot spot. spacecraft docking electromagnetic formation flight dynamics and control is the direction of the first spacecraft docking electromagnetic formation flight dynamics and control . the system introduces the electromagnetic state of the art docking of spacecraft flying in formation. kinet.…