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Relevant bibliographies by topics / Guidance and Control Algorithm Design

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Dissertations / Theses
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Academic literature on the topic 'Guidance and Control Algorithm Design'

Author: Grafiati

Published: 27 June 2021

Last updated: 29 July 2025

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Journal articles on the topic "Guidance and Control Algorithm Design"

1

Ha, Cheol-Keun, and Hyoung-Sik Choi. "Design of Autolanding Guidance and Control Algorithm Using Singular Perturbation." Journal of Control, Automation and Systems Engineering 11, no. 8 (2005): 726–32. http://dx.doi.org/10.5302/j.icros.2005.11.8.726.

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Ali, Syed Ussama, Raza Samar, M. Zamurad Shah, Aamer I. Bhatti, and Khalid Munawar. "Higher-order sliding mode based lateral guidance for unmanned aerial vehicles." Transactions of the Institute of Measurement and Control 39, no. 5 (2015): 715–27. http://dx.doi.org/10.1177/0142331215619972.

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A nonlinear sliding mode based scheme is developed for lateral guidance of unmanned aerial vehicles. The guidance and control system is considered as an inner and outer loop design problem, the outer guidance loop generates commands for the inner control loop to follow. Control loop dynamics is considered during derivation of the guidance logic, along with saturation constraints on the guidance commands. A nonlinear sliding manifold is selected for guidance logic design, the guidance loop generates bank angle commands for the inner roll control loop to follow. The real twisting algorithm, a hi

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Leng, Gerard. "Guidance Algorithm Design: A Nonlinear Inverse Approach." Journal of Guidance, Control, and Dynamics 21, no. 5 (1998): 742–46. http://dx.doi.org/10.2514/2.4300.

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Peng, Huei, and Masayoshi Tomizuka. "Preview Control for Vehicle Lateral Guidance in Highway Automation." Journal of Dynamic Systems, Measurement, and Control 115, no. 4 (1993): 679–86. http://dx.doi.org/10.1115/1.2899196.

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The continuous time deterministic optimal preview control algorithm is applied to the lateral guidance of a vehicle for an automated highway. In the lateral guidance problem, the front wheel steering angle of the vehicle is controlled so that the vehicle follows the center for a lane with small tracking error and maintains good ride quality simultaneously. A preview control algorithm is obtained by minimizing a quadratic performance index which includes terms representing the passenger ride quality as well as the lateral tracking error, each of these terms is multiplied by a frequency dependen

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Chao, Tao, Denghui Zhang, Songyan Wang, and Ping Ma. "Integrated guidance and control design considering system uncertainty." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 233, no. 6 (2018): 2278–90. http://dx.doi.org/10.1177/0954410018776512.

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The hypersonic vehicle has the characteristics of strong coupling, high uncertainty and complex nonlinearity, leading to an unsatisfactory control performance with the traditional design method. In this paper, an integrated guidance and control design approach is proposed to cope with this problem. A time-varying longitudinal integrated guidance and control model is first formulated, and then the overall uncertainty consisting of the un-modeled dynamic, parameter uncertainty and external disturbance is taken into account. A novel finite-time extended state observer is developed to estimate and

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Dentis, Matteo, Elisa Capello, and Giorgio Guglieri. "A Novel Concept for Guidance and Control of Spacecraft Orbital Maneuvers." International Journal of Aerospace Engineering 2016 (2016): 1–14. http://dx.doi.org/10.1155/2016/7695257.

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The purpose of this paper is the design of guidance and control algorithms for orbital space maneuvers. A 6-dof orbital simulator, based on Clohessy-Wiltshire-Hill equations, is developed in C language, considering cold gas reaction thrusters and reaction wheels as actuation system. The computational limitations of on-board computers are also included. A combination of guidance and control algorithms for an orbital maneuver is proposed: (i) a suitably designed Zero-Effort-Miss/Zero-Effort-Velocity (ZEM/ZEV) algorithm is adopted for the guidance and (ii) a linear quadratic regulator (LQR) is us

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Tran, Huy Ngoc, Thanh Nguyen Nhut Pham, and Bao Hong Thai Vo. "A study on tracking controller design for unmanned surface vehicles using magnetic coupling thruster." Science and Technology Development Journal 20, K5 (2017): 64–72. http://dx.doi.org/10.32508/stdj.v20ik5.1161.

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Controlling the unmanned surface vehicles to follow the object or define trajectory have many important applications in the field as military, survey quality environment so this problem has been much research on the world. This report represents the method to control the unmanned surface vehicles which use thruster with coupling follow square or zig-zag trajectories using the Line of Sight (LOS) algorithm combined with the Backstepping Controller. The system consists of three main blocks, Guidance - Control - Ship. Guidance will help to select waypoints to create the trajectory the use the LOS

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Wang, Hongbin, Jiao Dong, Zhikun Liu, Li Yan, and Shiqi Wang. "Control Algorithm for Trajectory Tracking of an Underactuated USV under Multiple Constraints." Mathematical Problems in Engineering 2022 (May 5, 2022): 1–12. http://dx.doi.org/10.1155/2022/5274452.

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A trajectory tracking control method based on the cascade of optimal guidance and adaptive control laws was proposed for trajectory tracking of an unmanned surface vehicle under multiple motion constraints including an ocean current disturbance environment. Considering the velocity and acceleration constraints, angular velocity, and angular acceleration constraints in guidance law design, motion planning was conducted with three degrees of freedom using a motion model and predictive control, while optimal guidance law was designed through a rolling optimization strategy to stabilize the positi

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Fu, Zhenhua, Kuanqiao Zhang, Qintao Gan, and Suochang Yang. "Integrated Guidance and Control with Input Saturation and Impact Angle Constraint." Discrete Dynamics in Nature and Society 2020 (September 15, 2020): 1–19. http://dx.doi.org/10.1155/2020/5917983.

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Aiming at the problem of impact angle constraint and input saturation, an integrated guidance and control (IGC) algorithm with impact angle constraint and input saturation is proposed. A three-channel independent design model of missile IGC with impact angle constraint is established, and an extended state observer with fast finite-time convergence is designed to estimate and compensate model errors and coupling relationship between channels. Based on the nonsingular terminal sliding mode control and backstepping control, the IGC three-channel independent design is completed. Nussbaum function

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Wang, Wenwen, Mingyu Wu, Zhihua Chen, and Xiaoli Liu. "Integrated Guidance-and-Control Design for Three-Dimensional Interception Based on Deep-Reinforcement Learning." Aerospace 10, no. 2 (2023): 167. http://dx.doi.org/10.3390/aerospace10020167.

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This study applies deep-reinforcement-learning algorithms to integrated guidance and control for three-dimensional, high-maneuverability missile-target interception. Dynamic environment, reward functions concerning multi-factors, agents based on the deep-deterministic-policy-gradient algorithm, and action signals with pitch and yaw fins as control commands were constructed in the research, which control the missile in order to intercept targets. Firstly, the missile-interception system includes dynamics such as the inertia of the missile, the aerodynamic parameters, and fin delays. Secondly, t

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Dissertations / Theses on the topic "Guidance and Control Algorithm Design"

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Chomel, Christina T. (Christina Tvrdik) 1973. "Design of a robust integrated guidance and control algorithm for the landing of an autonomous reusable launch vehicle." Thesis, Massachusetts Institute of Technology, 1998. http://hdl.handle.net/1721.1/9940.

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Bruno, Liam T. "Three Axis Attitude Control System Design and Analysis Tool Development for the Cal Poly CubeSat Laboratory." DigitalCommons@CalPoly, 2020. https://digitalcommons.calpoly.edu/theses/2288.

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The Cal Poly CubeSat Laboratory (CPCL) is currently facing unprecedented engineering challenges—both technically and programmatically—due to the increasing cost and complexity of CubeSat flight missions. In responding to recent RFPs, the CPCL has been forced to find commercially available solutions to entire mission critical spacecraft subsystems such as propulsion and attitude determination & control, because currently no in-house options exist for consideration. The commercially available solutions for these subsystems are often extremely expensive and sometimes provide excessively good perf

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Gagliano, Joseph R. "Orbital Constellation Design and Analysis Using Spherical Trigonometry and Genetic Algorithms: A Mission Level Design Tool for Single Point Coverage on Any Planet." DigitalCommons@CalPoly, 2018. https://digitalcommons.calpoly.edu/theses/1877.

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Recent interest surrounding large scale satellite constellations has increased analysis efforts to create the most efficient designs. Multiple studies have successfully optimized constellation patterns using equations of motion propagation methods and genetic algorithms to arrive at optimal solutions. However, these approaches are computationally expensive for large scale constellations, making them impractical for quick iterative design analysis. Therefore, a minimalist algorithm and efficient computational method could be used to improve solution times. This thesis will provide a tool for si

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Hallberg, Eric N. "On integrated plant, control and guidance design." Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 1997. http://handle.dtic.mil/100.2/ADA341957.

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Dissertation (Ph.D. in Aeronautics and Astronautics) Naval Postgraduate School, September 1997.<br>"September 1997." Dissertation supervisor(s): Isaac I. Kaminer. Includes bibliographical references (p. 187-190). Also available online.

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Moon, Jongki. "Mission-based guidance system design for autonomous UAVs." Diss., Atlanta, Ga. : Georgia Institute of Technology, 2009. http://hdl.handle.net/1853/31797.

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Thesis (Ph.D)--Aerospace Engineering, Georgia Institute of Technology, 2010.<br>Committee Chair: Prasad, JVR; Committee Member: Costello, Mark; Committee Member: Johnson, Eric; Committee Member: Schrage, Daniel; Committee Member: Vela, Patricio. Part of the SMARTech Electronic Thesis and Dissertation Collection.

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Maskey, Anuj. "Battery energy storage system control algorithm design." Thesis, Maskey, Anuj (2019) Battery energy storage system control algorithm design. Honours thesis, Murdoch University, 2019. https://researchrepository.murdoch.edu.au/id/eprint/52653/.

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Microgrid is based on smaller decentralised low voltage system with the use of modern power technology puts different types of Distributed Energy sources solar power, wind power, and energy storage devices together, improving the electrical supply reliability, reducing the feeder loss and ensures the stability of the voltage. The current trend of incorporating energy storage devices in the microgrid is aimed to mitigate the power imbalance and improve the electrical supply reliability. The thesis uses Kalbarri, Western Australia as a case study site with an aim to investigate the appropriate b

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Brown, Derek William. "Systolic algorithm design for control and signal processing." Thesis, Queen's University Belfast, 1996. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.337644.

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Li, Ming-Yan. "Performance analysis and enhancement of proportional navigation guidance systems /." Title page, table of contents and abstract only, 1999. http://web4.library.adelaide.edu.au/theses/09ENS/09ensl693.pdf.

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Isiyel, Kadir. "Autopilot Design And Guidance Control Of Ulisar Uuv (unmanned Underwater Vehicle)." Master's thesis, METU, 2007. http://etd.lib.metu.edu.tr/upload/12608867/index.pdf.

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Unmanned Underwater Vehicles (UUV) in open-seas are highly nonlinear with system motions. Because of the complex interaction of the body with environment it is difficult to control them efficiently. Linearization is applied to system in order to design controllers developed for linear systems. To overcome the effects of disturbances, a mathematical model which will compensate all disturbances and effects of linearization is required. In this study first a mathematical model is formed wherein the linear and nonlinear hydrodynamic coeffi- cients are calculated with strip theory. After the basic

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Morgan, H. P. "Quantitative design guidance on smoke control in shopping malls and atria." Thesis, London South Bank University, 1993. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.618632.

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Books on the topic "Guidance and Control Algorithm Design"

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Froncillo, Steven J. Design of digital control algorithms for unmanned air vehicles. Naval Postgraduate School, 1998.

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A, Dukeman G., and United States. National Aeronautics and Space Administration., eds. Examination of a practical aerobraking guidance algorithm. American Institute of Aeronautics and Astronautics, 1995.

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Zhang, Zhonghua. Smart TCT: An efficient algorithm for supervisory control design. National Library of Canada, 2001.

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United States. National Aeronautics and Space Administration., ed. The minimal time detection algorithm. National Aeronautics and Space Administration, 1995.

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Harald, Buschek, Calise Anthony J, and United States. National Aeronautics and Space Administration., eds. Homotopy algorithm for fixed order mixed H₂/H[infinity] design. National Aeronautics and Space Administration, 1996.

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6

Hallberg, Eric N. On integrated plant, control and guidance design. Naval Postgraduate School, 1997.

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7

Allen, Cheryl L. Guidance, navigation, and control subsystem equipment selection algorithm using expert system methods. Langley Research Center, 1991.

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United States. National Aeronautics and Space Administration., ed. Entry vehicle performance analysis and atmospheric guidance algorithm for precision landing on Mars. The Charles Stark Draper Laboratory, Inc., 1990.

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Council, Winchester (England) City, ed. Design guidance for the control of shopfronts & signs. Winchester City Council, 1998.

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Danley, D. R. Development of photovoltaic-diesel hybrid system design incorporating advanced control algorithm. The Branch, 1990.

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Book chapters on the topic "Guidance and Control Algorithm Design"

1

Hochstrasser, Markus, Simon P. Schatz, Kajetan Nürnberger, Markus Hornauer, Stephan Myschik, and Florian Holzapfel. "Aspects of a Consistent Modeling Environment for DO-331 Design Model Development of Flight Control Algorithms." In Advances in Aerospace Guidance, Navigation and Control. Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-65283-2_4.

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Zhao, Dangjun, Zhiwei Zhang, and Mingzhen Gui. "Birkhoff Pseudospectral Method and Convex Programming for Trajectory Optimization." In Autonomous Trajectory Planning and Guidance Control for Launch Vehicles. Springer Nature Singapore, 2023. http://dx.doi.org/10.1007/978-981-99-0613-0_4.

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AbstractTrajectory optimization, an optimal control problem (OCP) in essence, is an important issue in many engineering applications including space missions, such as orbit insertion of launchers, orbit rescue, formation flying, etc. There exist two kinds of solving methods for OCP, i.e., indirect and direct methods. For some simple OCPs, using the indirect methods can result in analytic solutions, which are not easy to be obtained for complicated systems. Direct methods transcribe an OCPs into a finite-dimensional nonlinear programming (NLP) problem via discretizing the states and the control

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Suresh, B. N., and K. Sivan. "Navigation Guidance and Control System." In Integrated Design for Space Transportation System. Springer India, 2015. http://dx.doi.org/10.1007/978-81-322-2532-4_14.

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Isermann, Rolf. "Computer-aided Control Algorithm Design." In Digital Control Systems. Springer Berlin Heidelberg, 1991. http://dx.doi.org/10.1007/978-3-642-86420-9_19.

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Liu, Jinkun. "Intelligent Search Algorithm Design." In Intelligent Control Design and MATLAB Simulation. Springer Singapore, 2017. http://dx.doi.org/10.1007/978-981-10-5263-7_11.

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Hoffmann, Arndt, Kai Loftfield, and Robert Luckner. "Broadband Wind Estimation Algorithm for Gust Load Alleviation." In Advances in Aerospace Guidance, Navigation and Control. Springer Berlin Heidelberg, 2011. http://dx.doi.org/10.1007/978-3-642-19817-5_25.

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Kownacki, Cezary, and Daniel Ołdziej. "Flocking Algorithm for Fixed-Wing Unmanned Aerial Vehicles." In Advances in Aerospace Guidance, Navigation and Control. Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-17518-8_24.

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Theuma, Kevin, and David Zammit Mangion. "An Image Processing Algorithm for Ground Navigation of Aircraft." In Advances in Aerospace Guidance, Navigation and Control. Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-17518-8_22.

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Tokhi, M. O., M. A. Hossain, and M. H. Shaheed. "Algorithm Analysis and Design." In Parallel Computing for Real-time Signal Processing and Control. Springer London, 2003. http://dx.doi.org/10.1007/978-1-4471-0087-4_6.

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Fischer, Raymond, and Leonid Boroditsky. "Design Guidance, Do’s and Dont’s, and Optimized Solutions." In Noise and Vibration Control on Ships. Springer Nature Switzerland, 2024. http://dx.doi.org/10.1007/978-3-031-55170-3_10.

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Conference papers on the topic "Guidance and Control Algorithm Design"

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Chen, Tianle, Mingwen Li, and Xiaoguang Jiao. "Integrated Design of Guidance and Control Algorithm Considering Multiple Constraints." In 2025 8th International Conference on Advanced Algorithms and Control Engineering (ICAACE). IEEE, 2025. https://doi.org/10.1109/icaace65325.2025.11020355.

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Huang, Mei, and Rui Hu. "Design of a College Student Employment Guidance Platform Based on Spark Framework and FP Growth Algorithm." In 2024 8th International Symposium on Computer Science and Intelligent Control (ISCSIC). IEEE, 2024. https://doi.org/10.1109/iscsic64297.2024.00027.

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Hu, Botao, and Sandipan Mishra. "Time-optimal Trajectory Planning for Landing Onto Moving Platforms." In Vertical Flight Society 73rd Annual Forum & Technology Display. The Vertical Flight Society, 2017. http://dx.doi.org/10.4050/f-0073-2017-12203.

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In this paper, an algorithm for time-optimal trajectory generation is developed for landing a 6 degree-of-freedom (DOF) quadrotor onto a moving platform (with tilt, heave and pitch). The overall control architecture has a standard guidance-and-tracking control inner-outer loop structure. The outer loop (guidance control) solves the time-optimal trajectory generation problem. Instead of directly solving the time-optimal control problem, the proposed method reformulates this into a nonlinear programming problem that transforms the constraints on the original system dynamics and inputs onto const

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Park, Kihong, and Mark Psiaki. "Design and test of a parallel trajectory optimization algorithm." In Guidance, Navigation, and Control Conference. American Institute of Aeronautics and Astronautics, 1994. http://dx.doi.org/10.2514/6.1994-3636.

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Calise, Anthony, Nahum Melamed, Seungjae Lee, Anthony Calise, Nahum Melamed, and Seungjae Lee. "Design and evaluation of a 3-D optimal ascent guidance algorithm." In Guidance, Navigation, and Control Conference. American Institute of Aeronautics and Astronautics, 1997. http://dx.doi.org/10.2514/6.1997-3707.

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Perhinschi, Mario, and Mario Perhinschi. "A modified genetic algorithm for the design of autonomous helicopter control system." In Guidance, Navigation, and Control Conference. American Institute of Aeronautics and Astronautics, 1997. http://dx.doi.org/10.2514/6.1997-3630.

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Lee, Dongwoo, Seung-Keun Kim, and Jinyoung Suk. "Design of a Track Guidance Algorithm for Formation Flight of UAVs." In AIAA Guidance, Navigation, and Control Conference. American Institute of Aeronautics and Astronautics, 2015. http://dx.doi.org/10.2514/6.2015-1315.

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DOTY, KARL. "A multiple algorithm solution to the AIAA GN & C Artificial Intelligence Design Challenge." In Guidance, Navigation and Control Conference. American Institute of Aeronautics and Astronautics, 1987. http://dx.doi.org/10.2514/6.1987-2329.

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Hoffmann, Falk. "FCS Notch Filter Design Using Genetic/Evolutionary Algorithm." In AIAA Guidance, Navigation, and Control Conference and Exhibit. American Institute of Aeronautics and Astronautics, 2004. http://dx.doi.org/10.2514/6.2004-4758.

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Kerr, Murray, Rodrigo Haya, Luis Peñín, Gabriele De Zaiacomo, David Mostaza, and Victor Marco. "IXV Re-entry Guidance, Control & DRS Triggering: Algorithm Design and Assessment." In AIAA Guidance, Navigation, and Control Conference. American Institute of Aeronautics and Astronautics, 2012. http://dx.doi.org/10.2514/6.2012-4841.

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Reports on the topic "Guidance and Control Algorithm Design"

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Dohner, J. L. A guidance and control algorithm for scent tracking micro-robotic vehicle swarms. Office of Scientific and Technical Information (OSTI), 1998. http://dx.doi.org/10.2172/573345.

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Gebre-Egziabher, Demoz. An Integrated Design Methodology for Nanosat Navigation Guidance and Control Systems. Defense Technical Information Center, 2007. http://dx.doi.org/10.21236/ada474558.

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Weinger, Matthew B., and Clinton Brown. Meta-Level Design Guidance and Operator Performance Measures for Hybrid Control Rooms. Office of Scientific and Technical Information (OSTI), 2018. http://dx.doi.org/10.2172/1475171.

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Thomas Ulrich, Ronald Boring, William Phoenix, et al. Applying Human Factors Evaluation and Design Guidance to a Nuclear Power Plant Digital Control System. Office of Scientific and Technical Information (OSTI), 2012. http://dx.doi.org/10.2172/1082368.

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Hernandez, J., R. Smith, V. Petty, and J. Lock. Development of Range Design Elements and Quality Control/Quality Assurance Guidance to Reduce Maintenance Requirements on Training Ranges. Defense Technical Information Center, 2006. http://dx.doi.org/10.21236/ada460751.

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Blodgett, Douglas, Michael Behnke, and William Erdman. Power Converter Control Algorithm Design and Simulation for the NREL Next-Generation Drivetrain: July 8, 2013 - January 7, 2016. Office of Scientific and Technical Information (OSTI), 2016. http://dx.doi.org/10.2172/1318194.

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R. Fink, D. Hill, J. O'Hara. Human Factors Guidance for Control Room and Digital Human-System Interface Design and Modification, Guidelines for Planning, Specification, Design, Licensing, Implementation, Training, Operation and Maintenance. Office of Scientific and Technical Information (OSTI), 2004. http://dx.doi.org/10.2172/835085.

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Wenren, Yonghu, Joon Lim, Luke Allen, Robert Haehnel, and Ian Dettwiler. Helicopter rotor blade planform optimization using parametric design and multi-objective genetic algorithm. Engineer Research and Development Center (U.S.), 2022. http://dx.doi.org/10.21079/11681/46261.

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In this paper, an automated framework is presented to perform helicopter rotor blade planform optimization. This framework contains three elements, Dakota, ParBlade, and RCAS. These elements are integrated into an environment control tool, Galaxy Simulation Builder, which is used to carry out the optimization. The main objective of this work is to conduct rotor performance design optimizations for forward flight and hover. The blade design variables manipulated by ParBlade are twist, sweep, and anhedral. The multi-objective genetic algorithm method is used in this study to search for the optim

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Thompson and Lawson. L51691 Fracture Control Technology for Natural Gas Pipelines. Pipeline Research Council International, Inc. (PRCI), 1993. http://dx.doi.org/10.55274/r0011368.

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Operational integrity of gas-transmission pipelines is a goal of all operators. Pipeline integrity is achieved by planning, controlling, and monitoring a number of elements, all of which contribute to the total pipeline system integrity. Elements that affect overall pipeline integrity are pipeline design, pipe specification, pipe transportation and handling, pipeline construction and inspection, preservice testing, and operation and maintenance practices. Fracture control is part of a number of these elements. This research report and software satisfies the industry need for a comprehensive de

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Bando, Rosangela. Guidelines for Impact Evaluation in Education Using Experimental Design. Inter-American Development Bank, 2013. http://dx.doi.org/10.18235/0009133.

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There has been extensive research and investment in strategies that aim to improve the quality of education around the world. But despite rigorous evidence, the question of what to do in a specific context usually remains only partially answered at best. As a result, numerous impact evaluations are being conducted with the goal of learning what works. The goal of the guidelines presented here is to summarize the evidence and provide references in a single document in order to save time for those implementing education impact evaluations through randomized control trials. The guidelines focus o

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