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    Nonlinear image-based visual servo controller for automatic landing guidance of a fixed-wing aircraft

    Bras, Florent Le / Hamel, Tarek / Barat, Christian et al. | Tema Archiv | 2009
    the airplane guidance problem to derive a control Lyapunov function along with an estimate of the wind gust. Finally simulation results are ...

    Automated model analysis and test generation for flight guidance mode logic

    Busser, R.D. / Blackburn, M.R. / Nauman, A.M. | Tema Archiv | 2001
    to develop the mode control logic of a Flight Guidance System (FGS) for a General Aviation class aircraft Rockwell Collins later used an ...

    Control Strategies for Flexible Joint Manipulators

    Ulrich, S. / Sasiadek, J. / American Institute of Aeronautics and Astronautics; Conferderation of European Aerospace Societies | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Online Analytical Guidance for a Solid-Fuel Launch Vehicle in Boost Phase Based on Generalized Zero Effort Miss

    Yu, Qi / Chen, Wanchun / Wei, Hongkui et al. | IEEE | 2023
    online analytical guidance has the advantages of high accuracy and strong robustness. ...

    Nonlinear Generalized Dynamic Inversion Aircraft Control

    Hameduddin, I. / Bajodah, A. / American Institute of Aeronautics and Astronautics; Confederation of European Aerospace Societies | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Attitude Control Actuators for a Simulated Spacecraft

    McChesney, C. / American Institute of Aeronautics and Astronautics; Conferderation of European Aerospace Societies | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Derivative-Free Output Feedback Adaptive Control

    Yucelen, T. / Kim, K. / Calise, A. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Adaptive guidance systems for hypersonic reusable launch vehicles

    Schierman, J.D. / Ward, D.G. / Hull, J.R. et al. | IEEE | 2001
    the extent possible. However, nominal performance will typically not be fully recovered for RLV, and the outer-loop guidance system must ...

    Robust stochastic controller for a missile guidance system

    Rizk, M.R.M. / Rahim, M.A. | Tema Archiv | 2000
    guidance process equations are represented by the kinematic equations of motion of a missile, and approximate equations of rotary motion of a ...

    Improving positioning, guidance, system and communication technology of AVCS by optics

    Tsumura, T. | Tema Archiv | 1997
    approach and communication system for all functions by using laser and light beams and corner cubes. Regarding the positioning, guidance and ...
    Verlag: Institute of Electrical and Electronics Engineers (IEEE) , New York

    New weapon concepts developed from advances navigation guidance and targeting technology

    Brown, H.E. | Tema Archiv | 1978

    A new concept for integrated guidance and drive of railway running gears

    Gretzschel, M. / Bose, L. | Tema Archiv | 2000
    running stability at high velocities and steering of the vehicle with decrease of friction power and thus wear in curves. For vehicles with single ...

    The effect of haptic guidance on curve negotiation behavior of young, experienced drivers

    Mulder, M. / Abbink, D.A. / Boer, E.R. | Tema Archiv | 2008
    guidance based on the concept of shared control, where both the driver and the support system influence the steering wheel torque. The haptic ...

    State Limiter for Model Following Control Systems

    Gadient, R. / Lavretsky, E. / Hyde, D. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Modeling for Control of Very Flexible Aircraft

    Gibson, T. / Annaswamy, A. / Lavretsky, E. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Testing of RTK-level satellite-based tractor auto- guidance using a visual sensor system

    Easterley, Dwight / Adamchuk, Viacheslav / Hoy, Roger et al. | Tema Archiv | 2010
    include the automated steering of tractors and self-propelled machinery. With the development of auto-guidance systems comes the need to evaluate ...

    Fault/Damage Tolerant Control of a Quadrotor Helicopter UAV using Model Reference Adaptive Control and Gain-Scheduled PID

    Sadeghzadeh, I. / Mehta, A. / Zhang, Y. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Fin Mixing Optimization to Minimize Control Coupling Effects

    Kutluay, U. / American Institute of Aeronautics and Astronautics; Conferderation of European Aerospace Societies | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Further Results Towards a Location-Scheduled Control Methodology

    Sorgenfrei, M. / Joshi, S. / American Institute of Aeronautics and Astronautics; Conferderation of European Aerospace Societies | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    A Method For Enforcing State Constraints in Adaptive Control

    Muse, J. / American Institute of Aeronautics and Astronautics; Conferderation of European Aerospace Societies | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Guidance and navigation for automatic landing, rollout, and turnoff using MLS and magnetic cable sensors

    Pines, S. / Hueschen, R.M. | Tema Archiv | 1978

    Dynamic congestion pricing based on traffic guidance with Kalman filtering theory

    Sheng Li, | IEEE | 2002

    Model Predictive Control Scheme for Rotorcraft Inverse Simulation

    Avanzini, G. / Thomson, D. / Torasso, A. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Spherical Air Bearing Attitude Control Simulator for Nanosatellites

    Ustrzycki, T. / Lee, R. / Chesser, H. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    PDE Boundary Control for Flexible Articulated Aircraft Wings

    Paranjape, A. / Chung, S. / Krstic, M. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Torque-saturated, Inertia-Free Spacecraft Attitude Control

    Cruz, G. / Yang, X. / Weiss, A. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    A modified nonlinear guidance logic for a leader-follower formation flight of two UAVs

    Kim, Do-Myung / Nam, Suhyun / Suk, Jinyoung | Tema Archiv | 2009
    guidance algorithm provides a good performance and relatively simple control logic. The performance of the proposed guidance algorithm is tested ...

    Travel times as a basic part of the LISB guidance strategy

    Hoffmann, G. / Janko, J. | Tema Archiv | 1990
    The Berlin LISB Guidance and Information system is an individual, dynamic guidance system for motorised vehicles. LISB works in accordance ...
    Schlagwörter: BERLIN LISB GUIDANCE AND INFORMATION SYSTEM

    Multivariable design of a bank-to-turn autopilot for command guidance

    McConnell, G. / Irwin, G.W. | Tema Archiv | 1988
    lateral acceleration. The potential benefits arising include improved guidance loop performance and also the fact that, once designed, the ...
    Schlagwörter: AEROSPACE COMPUTER CONTROL , MULTIVARIABLE CONTROL SYSTEM DESIGN , COMMAND GUIDANCE , GUIDANCE LOOP PERFORMANCE , CLOS GUIDANCE LOOPS , TIME DOMAIN LINEAR QUADRATIC OPTIMAL CONTROL METHOD

    Fault-Tolerant Attitude Control of a Micro-Satellite using a Redundancy-Free Single Gimbal Variable Speed Control Moment Gyroscope (SGVSCMG) System

    Chandrasekar, S. / Hwang, I. / American Institute of Aeronautics and Astronautics; Conferderation of European Aerospace Societies | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Stability and Control of Ground Tethered Energy Systems

    Hussein, I. / Olinger, D. / Tryggvason, G. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Adaptive Control of an Elastic General Aviation Aircraft

    Hinson, B. / Steck, J. / Rokhsaz, K. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Fault Tolerant Control of an Over Actuated UAV

    Isik, S. / Tekinalp, O. / Yavrucuk, I. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Gust Load Alleviation Control for Very Flexible Aircraft

    Dillsaver, M. / Cesnik, C. / Kolmanovsky, I. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Control Oriented Modeling of 6-DOF Hypersonic Vehicle Dynamics

    Shakiba, M. / Serrani, A. / American Institute of Aeronautics and Astronautics; Conferderation of European Aerospace Societies | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Fault-Tolerant Adaptive Flight Control System Using Feedback Linearization

    Namba, T. / Uchiyama, K. / American Institute of Aeronautics and Astronautics; Conferderation of European Aerospace Societies | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Development and Construction of Intelligent Vehicle Loading Management and Control System

    Lu, Ning / Wang, Xuelin / Zhang, Zhaolun et al. | IEEE | 2023
    and guidance module, remote control and monitoring module to achieves closed-loop linkage of loading operations and comprehensive management ...

    Formally specifying the logic of an automatic guidance controller

    Guaspari, D. | Tema Archiv | 1991
    the Advanced Transport Operating Systems program. It is used as a laboratory to study the development, implementation, and certification of ...
    Schlagwörter: NASA (NATIONAL AERONAUTICS AND SPACE ADMINISTRATION)

    Nonlinear Dynamic Inversion Baseline Control Law: Architecture and Performance Predictions

    Miller, C. / American Institute of Aeronautics and Astronautics; Conferderation of European Aerospace Societies | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Modelling and Multivariable Control Techniques for Small Coaxial Helicopters

    Mukherjee, P. / Waslander, S. / American Institute of Aeronautics and Astronautics; Conferderation of European Aerospace Societies | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Hybrid Control System for a Future Small Aircraft

    Heller, M. / Schuck, F. / Peter, L. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    A method for agricultural machine guidance on row crops based on the vanishing point

    de Oliveira Neris, Luciano / Obac Roda, Valentin / Trindade, Onofre | IEEE | 2007
    Automatic guidance systems have became important in agriculture to reduce the operator’s work and fatigue, resulting in higher ...

    Adaptive Estimation Based Loss of Control Detection and Mitigation

    Stepanyan, V. / Krishnakumar, K. / Barlow, J. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Active Flatness Fuzzy Logic Control of Space Membrane Structure

    Shan, J. / Orszulik, R. / Wenderski, P. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Route guidance system for automobile drivers by speech synthesis

    Tsugawa, S. / Tabei, S. | Tema Archiv | 1987
    This paper describes a route guidance system for automobile drivers by speech synthesis and road-vehicle digital communication. The system ...

    Design and Flight Testing of Manual Nonlinear Flight Control Laws

    Lombaerts, T. / Looye, G. / American Institute of Aeronautics and Astronautics; Conferderation of European Aerospace Societies | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    In-vehicle route guidance in the United States: 1910-1985

    French, R.L. | Tema Archiv | 1986
    ), and it enables map matching, which breathes new life into dead reckoning techniques that are many centuries older than the automobile. ...

    Analysis of Aircraft Multiple Engine Configurations for Fault Tolerant Control

    Perhinschi, M. / Beamer, F. / American Institute of Aeronautics and Astronautics; Conferderation of European Aerospace Societies | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Intelligent Control for Drag Reduction on the X-48B Vehicle

    Griffin, B. / Brown, N. / Yoo, S. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

    Application of Structural Load Feedback in Flight Control

    Frost, S. / Trinh, K. / Taylor, B. et al. | British Library Conference Proceedings | 2011
    Verlag: American Institute of Aeronautics and Astronautics , Reston, Va.

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