var bibbase_data = {"data":"<img src=\"//bibbase.org/img/ajax-loader.gif\" id=\"spinner\"\n  style=\"display: none;\" alt=\"Loading..\" />\n\n<div id=\"bibbase\">\n\n  <script type=\"text/javascript\">\n    var bibbase = {\n      params: {\"bib\":\"https://malik-nauman-rauf-207.github.io/Publications.bib\",\"jsonp\":\"1\",\"host\":\"bibbase.org\",\"ssl\":false},\n      data: [{\"bibtype\":\"inproceedings\",\"type\":\"inproceedings\",\"author\":[{\"propositions\":[],\"lastnames\":[\"Rauf\"],\"firstnames\":[\"Malik\",\"Nauman\"],\"suffixes\":[]},{\"propositions\":[],\"lastnames\":[\"Khan\"],\"firstnames\":[\"Roohan\",\"Ahmed\"],\"suffixes\":[]},{\"propositions\":[],\"lastnames\":[\"Ali\",\"Shah\"],\"firstnames\":[\"Syed\",\"Irtiza\"],\"suffixes\":[]}],\"booktitle\":\"2023 3rd International Conference on Digital Futures and Transformative Technologies (ICoDT2)\",\"title\":\"Stability Analysis & Development of a Control Strategy for a Small UAV\",\"year\":\"2023\",\"volume\":\"\",\"number\":\"\",\"pages\":\"1-6\",\"keywords\":\"Analytical models;Control design;Atmospheric modeling;Autonomous aerial vehicles;Controllability;Stability analysis;Frequency division multiplexing;UAV;Stability;Vortex-lattice Method;Dynamics Modeling;Control Implementation;Feedback Control;LQR\",\"doi\":\"10.1109/ICoDT259378.2023.10325756\",\"bibtex\":\"@INPROCEEDINGS{10325756,\\r\\n\\tauthor={Rauf, Malik Nauman and Khan, Roohan Ahmed and Ali Shah, Syed Irtiza},\\r\\n\\tbooktitle={2023 3rd International Conference on Digital Futures and Transformative Technologies (ICoDT2)}, \\r\\n\\ttitle={Stability Analysis & Development of a Control Strategy for a Small UAV}, \\r\\n\\tyear={2023},\\r\\n\\tvolume={},\\r\\n\\tnumber={},\\r\\n\\tpages={1-6},\\r\\n\\tkeywords={Analytical models;Control design;Atmospheric modeling;Autonomous aerial vehicles;Controllability;Stability analysis;Frequency division multiplexing;UAV;Stability;Vortex-lattice Method;Dynamics Modeling;Control Implementation;Feedback Control;LQR},\\r\\n\\tdoi={10.1109/ICoDT259378.2023.10325756}}\\r\\n\\r\\n\\r\\n\",\"author_short\":[\"Rauf, M. N.\",\"Khan, R. A.\",\"Ali Shah, S. I.\"],\"key\":\"10325756\",\"id\":\"10325756\",\"bibbaseid\":\"rauf-khan-alishah-stabilityanalysisdevelopmentofacontrolstrategyforasmalluav-2023\",\"role\":\"author\",\"urls\":{},\"keyword\":[\"Analytical models;Control design;Atmospheric modeling;Autonomous aerial vehicles;Controllability;Stability analysis;Frequency division multiplexing;UAV;Stability;Vortex-lattice Method;Dynamics Modeling;Control Implementation;Feedback Control;LQR\"],\"metadata\":{\"authorlinks\":{\"rauf, m\":\"https://maliknaumanrauf.me/publications.html\"}},\"html\":\"\"},{\"bibtype\":\"article\",\"type\":\"article\",\"abstract\":\"Developing a suitable flight dynamics model (FDM) by assessing the stability and controllability characteristics of the aircraft is essential during the conceptual and preliminary design phase, as it enables us to proceed with further analysis of loads endured and maneuverability aspects. In this paper, a strategy for computing the stability parameters of a small-scale loitering unmanned aerial vehicle (UAV) with a selected wing span employing two different stability analysis tools is presented, followed by the implementation of a sizing methodology for control surface sizing, which were selected as ailerons and ruddervators. Subsequently, the control integrated dynamics model is subjected to control input testing to evaluate the stability and control capabilities. The results indicate only a minor discrepancy between the stability results both the tools, with the overall aircraft being statically, and dynamically stable. Furthermore, the designed control surfaces satisfy the critical requirements and are able to adequately follow and react to the input commands. This study carries a great deal of significance for the stability and especially control design engineers working in the domain of UAV design as it presents simple method for developing a complete 6-degree-of-freedom(6-DOF) FDM.\",\"author\":[{\"firstnames\":[\"Malik\",\"Nauman\"],\"propositions\":[],\"lastnames\":[\"Rauf\"],\"suffixes\":[]},{\"firstnames\":[\"·\"],\"propositions\":[],\"lastnames\":[\"Roohan\"],\"suffixes\":[]},{\"firstnames\":[\"Ahmed\"],\"propositions\":[],\"lastnames\":[\"Khan\"],\"suffixes\":[]},{\"firstnames\":[\"·\"],\"propositions\":[],\"lastnames\":[\"Syed\"],\"suffixes\":[]},{\"firstnames\":[\"Irtiza\",\"Ali\"],\"propositions\":[],\"lastnames\":[\"Shah\"],\"suffixes\":[]},{\"firstnames\":[\"·\"],\"propositions\":[],\"lastnames\":[\"Messam\"],\"suffixes\":[]},{\"firstnames\":[\"Abbas\"],\"propositions\":[],\"lastnames\":[\"Naqvi\"],\"suffixes\":[]}],\"doi\":\"10.1007/s40435-023-01322-2\",\"journal\":\"International Journal of Dynamics and Control\",\"keywords\":\"Athena AVL,Control implementation,Dynamics modeling,Stability,UAV,Vortex-lattice method,XFLR5\",\"pages\":\"1801-1816\",\"title\":\"Design and analysis of stability and control for a small unmanned aerial vehicle\",\"volume\":\"12\",\"url\":\"https://doi.org/10.1007/s40435-023-01322-2\",\"year\":\"2024\",\"bibtex\":\"@article{Rauf2024,\\r\\n\\tabstract = {Developing a suitable flight dynamics model (FDM) by assessing the stability and controllability characteristics of the aircraft is essential during the conceptual and preliminary design phase, as it enables us to proceed with further analysis of loads endured and maneuverability aspects. In this paper, a strategy for computing the stability parameters of a small-scale loitering unmanned aerial vehicle (UAV) with a selected wing span employing two different stability analysis tools is presented, followed by the implementation of a sizing methodology for control surface sizing, which were selected as ailerons and ruddervators. Subsequently, the control integrated dynamics model is subjected to control input testing to evaluate the stability and control capabilities. The results indicate only a minor discrepancy between the stability results both the tools, with the overall aircraft being statically, and dynamically stable. Furthermore, the designed control surfaces satisfy the critical requirements and are able to adequately follow and react to the input commands. This study carries a great deal of significance for the stability and especially control design engineers working in the domain of UAV design as it presents simple method for developing a complete 6-degree-of-freedom(6-DOF) FDM.},\\r\\n\\tauthor = {Malik Nauman Rauf and · Roohan and Ahmed Khan and · Syed and Irtiza Ali Shah and · Messam and Abbas Naqvi},\\r\\n\\tdoi = {10.1007/s40435-023-01322-2},\\r\\n\\tjournal = {International Journal of Dynamics and Control},\\r\\n\\tkeywords = {Athena AVL,Control implementation,Dynamics modeling,Stability,UAV,Vortex-lattice method,XFLR5},\\r\\n\\tpages = {1801-1816},\\r\\n\\ttitle = {Design and analysis of stability and control for a small unmanned aerial vehicle},\\r\\n\\tvolume = {12},\\r\\n\\turl = {https://doi.org/10.1007/s40435-023-01322-2},\\r\\n\\tyear = {2024}\\r\\n}\\r\\n\\r\\n\\r\\n\\r\\n\\r\\n\",\"author_short\":[\"Rauf, M. N.\",\"Roohan, ·\",\"Khan, A.\",\"Syed, ·\",\"Shah, I. A.\",\"Messam, ·\",\"Naqvi, A.\"],\"key\":\"Rauf2024\",\"id\":\"Rauf2024\",\"bibbaseid\":\"rauf-roohan-khan-syed-shah-messam-naqvi-designandanalysisofstabilityandcontrolforasmallunmannedaerialvehicle-2024\",\"role\":\"author\",\"urls\":{\"Paper\":\"https://doi.org/10.1007/s40435-023-01322-2\"},\"keyword\":[\"Athena AVL\",\"Control implementation\",\"Dynamics modeling\",\"Stability\",\"UAV\",\"Vortex-lattice method\",\"XFLR5\"],\"metadata\":{\"authorlinks\":{\"rauf, m\":\"https://maliknaumanrauf.me/publications.html\"}},\"downloads\":1,\"html\":\"\"},{\"bibtype\":\"article\",\"type\":\"article\",\"abstract\":\"Actual Structures are subjected to variable amplitude loading as opposed to a monotone. Many models have been proposed to study these effects analytically. The proposed study focuses on developing an algorithm, and a corresponding framework in MATLAB for two of these models, i.e. the NASGRO equation for constant amplitude loading, and Generalized Willenborg for overload effects. The overload influence is modelled by keeping track of changes in the crack-tip plastic-zone. Two cases are studied with the algorithm, and the results indicate that the presence of overload tends to retard crack growth, thereby validating our algorithm with literature findings.\",\"author\":[{\"firstnames\":[\"Malik\",\"Nauman\"],\"propositions\":[],\"lastnames\":[\"Rauf\"],\"suffixes\":[]},{\"firstnames\":[\"Rahma\"],\"propositions\":[],\"lastnames\":[\"Khan\"],\"suffixes\":[]},{\"firstnames\":[\"Gohar\"],\"propositions\":[],\"lastnames\":[\"Majeed\"],\"suffixes\":[]}],\"keywords\":\"Generalized Willenborg,MATLAB,NASGRO,Plastic Zone,Variable Amplitude Loading\",\"title\":\"Designing an Analysis Framework for Estimating Life of a Component Subjected to a Constant Load and a Single Overload Using MATLAB\",\"url\":\"https://www.researchgate.net/publication/365903636_Designing_an_Analysis_Framework_for_estimating_life_of_a_component_subjected_to_a_constant_load_and_a_single_overload_using_MATLAB\",\"year\":\"2023\",\"bibtex\":\"@article{Rauf2023,\\r\\n\\tabstract = {Actual Structures are subjected to variable amplitude loading as opposed to a monotone. Many models have been proposed to study these effects analytically. The proposed study focuses on developing an algorithm, and a corresponding framework in MATLAB for two of these models, i.e. the NASGRO equation for constant amplitude loading, and Generalized Willenborg for overload effects. The overload influence is modelled by keeping track of changes in the crack-tip plastic-zone. Two cases are studied with the algorithm, and the results indicate that the presence of overload tends to retard crack growth, thereby validating our algorithm with literature findings.},\\r\\n\\tauthor = {Malik Nauman Rauf and Rahma Khan and Gohar Majeed},\\r\\n\\tkeywords = {Generalized Willenborg,MATLAB,NASGRO,Plastic Zone,Variable Amplitude Loading},\\r\\n\\ttitle = {Designing an Analysis Framework for Estimating Life of a Component Subjected to a Constant Load and a Single Overload Using MATLAB},\\r\\n\\turl = {https://www.researchgate.net/publication/365903636_Designing_an_Analysis_Framework_for_estimating_life_of_a_component_subjected_to_a_constant_load_and_a_single_overload_using_MATLAB},\\r\\n\\tyear = {2023}\\r\\n}\\r\\n\\r\\n\\r\\n\\r\\n\",\"author_short\":[\"Rauf, M. N.\",\"Khan, R.\",\"Majeed, G.\"],\"key\":\"Rauf2023\",\"id\":\"Rauf2023\",\"bibbaseid\":\"rauf-khan-majeed-designingananalysisframeworkforestimatinglifeofacomponentsubjectedtoaconstantloadandasingleoverloadusingmatlab-2023\",\"role\":\"author\",\"urls\":{\"Paper\":\"https://www.researchgate.net/publication/365903636_Designing_an_Analysis_Framework_for_estimating_life_of_a_component_subjected_to_a_constant_load_and_a_single_overload_using_MATLAB\"},\"keyword\":[\"Generalized Willenborg\",\"MATLAB\",\"NASGRO\",\"Plastic Zone\",\"Variable Amplitude Loading\"],\"metadata\":{\"authorlinks\":{\"rauf, m\":\"https://maliknaumanrauf.me/publications.html\"}},\"downloads\":3,\"html\":\"\"}],\n      metadata: {\"owner\":\"rauf, m\",\"authorlinks\":{\"rauf, m\":\"https://maliknaumanrauf.me/publications.html\"}},\n      ownerID: \"7q6rBn9EYZ6RQ4q9N\"\n    };\n  </script>\n\n  <script type=\"text/javascript\">\n  var site$;\n  if (typeof $ != 'undefined') {\n    console.log('existing jquery: storing 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mVybG9hZF91c2luZ19NQVRMQUJ9LA0KCXllYXIgPSB7MjAyM30NCn0NCg0KDQoNCg==\">\n 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N.</a>; Roohan, ·; Khan, A.; Syed, ·; Shah, I. A.; Messam, ·;  and Naqvi, A.\n</span>\n\n  \n\n</span>\n\n  <i>International Journal of Dynamics and Control</i>, 12: 1801-1816.  2024.\n  <span class=\"note\"></span>\n\n<span class=\"bibbase_note\"></span>\n\n<br class=\"bibbase_paper_content\"/>\n\n<span class=\"bibbase_paper_content dontprint\">\n\n  \n  <a href=\"https://doi.org/10.1007/s40435-023-01322-2\"\n     onclick=\"log_download('rauf-roohan-khan-syed-shah-messam-naqvi-designandanalysisofstabilityandcontrolforasmallunmannedaerialvehicle-2024', 'https://doi.org/10.1007/s40435-023-01322-2', event.ctrlKey, event)\">\n    <img src=\"//bibbase.org/img/filetypes/link.svg\"\n\t     alt=\"Design and analysis of stability and control for a small unmanned aerial vehicle [link]\"\n       title=\"Paper\"\n       style=\"max-height: 1em;\"\n\t     class=\"bibbase_icon\"\n         ><span class=\"bibbase_icon_text\">Paper</span></a>\n  &nbsp;\n  \n\n  \n  <a href=\"http://doi.org/10.1007/s40435-023-01322-2\"\n     onclick=\"log_download('rauf-roohan-khan-syed-shah-messam-naqvi-designandanalysisofstabilityandcontrolforasmallunmannedaerialvehicle-2024', 'http://doi.org/10.1007/s40435-023-01322-2', event.ctrlKey)\"\n     class=\"bibbase doi link\">\n    <span>doi</span></a>\n  &nbsp;\n  \n\n  \n  <a href=\"//bibbase.org/network/publication/rauf-roohan-khan-syed-shah-messam-naqvi-designandanalysisofstabilityandcontrolforasmallunmannedaerialvehicle-2024\"\n     class=\"bibbase bibbase_page link\">link</a>\n  &nbsp;\n  \n\n  <a href=\"#\"\n     onclick=\"showBib(event); return false;\"\n     class=\"bibbase bibtex link\">bibtex\n    <i class=\"fa fa-caret-down\"></i></a>\n\n  \n  &nbsp;\n  <a class=\"bibbase_abstract_link bibbase link\"\n     href=\"#\"\n     onclick=\"showAbstract(event); return false;\">\n    abstract <i class=\"fa fa-caret-down\"></i></a>\n  \n\n  \n  &nbsp;\n  <span class=\"bibbase_stats_paper\" style=\"color: #777;\">\n    <span>1 download</span>\n  </span>\n  \n\n  <!-- <a class=\"bibbase read link hidden\" -->\n  <!--    href=\"javascript:toggleRead('rauf-roohan-khan-syed-shah-messam-naqvi-designandanalysisofstabilityandcontrolforasmallunmannedaerialvehicle-2024')\" -->\n  <!--    title=\"Marking this paper as read adds it to your library on BibBase.\" -->\n  <!--    > -->\n  <!--   <i class=\"fa fa-check\"></i>&nbsp; -->\n  <!--   <span>mark as read</span> -->\n  <!-- </a> -->\n\n  &nbsp;\n  \n  \n  \n  \n  \n  \n  \n  \n  \n  \n  \n  \n  \n  \n  \n  \n\n</span>\n\n<div class=\"well well-small bibbase\" data-type=\"bibtex\"\n     style=\"display:none\">\n  <pre style=\"white-space: pre-wrap;\">@article{Rauf2024,\r\n\tabstract = {Developing a suitable flight dynamics model (FDM) by assessing the stability and controllability characteristics of the aircraft is essential during the conceptual and preliminary design phase, as it enables us to proceed with further analysis of loads endured and maneuverability aspects. In this paper, a strategy for computing the stability parameters of a small-scale loitering unmanned aerial vehicle (UAV) with a selected wing span employing two different stability analysis tools is presented, followed by the implementation of a sizing methodology for control surface sizing, which were selected as ailerons and ruddervators. Subsequently, the control integrated dynamics model is subjected to control input testing to evaluate the stability and control capabilities. The results indicate only a minor discrepancy between the stability results both the tools, with the overall aircraft being statically, and dynamically stable. Furthermore, the designed control surfaces satisfy the critical requirements and are able to adequately follow and react to the input commands. This study carries a great deal of significance for the stability and especially control design engineers working in the domain of UAV design as it presents simple method for developing a complete 6-degree-of-freedom(6-DOF) FDM.},\r\n\tauthor = {Malik Nauman Rauf and · Roohan and Ahmed Khan and · Syed and Irtiza Ali Shah and · Messam and Abbas Naqvi},\r\n\tdoi = {10.1007/s40435-023-01322-2},\r\n\tjournal = {International Journal of Dynamics and Control},\r\n\tkeywords = {Athena AVL,Control implementation,Dynamics modeling,Stability,UAV,Vortex-lattice method,XFLR5},\r\n\tpages = {1801-1816},\r\n\ttitle = {Design and analysis of stability and control for a small unmanned aerial vehicle},\r\n\tvolume = {12},\r\n\turl = {https://doi.org/10.1007/s40435-023-01322-2},\r\n\tyear = {2024}\r\n}\r\n\r\n\r\n\r\n\r\n</pre>\n</div>\n\n\n<div class=\"well well-small bibbase\" data-type=\"abstract\"\n     style=\"display:none\">\n  Developing a suitable flight dynamics model (FDM) by assessing the stability and controllability characteristics of the aircraft is essential during the conceptual and preliminary design phase, as it enables us to proceed with further analysis of loads endured and maneuverability aspects. In this paper, a strategy for computing the stability parameters of a small-scale loitering unmanned aerial vehicle (UAV) with a selected wing span employing two different stability analysis tools is presented, followed by the implementation of a sizing methodology for control surface sizing, which were selected as ailerons and ruddervators. Subsequently, the control integrated dynamics model is subjected to control input testing to evaluate the stability and control capabilities. The results indicate only a minor discrepancy between the stability results both the tools, with the overall aircraft being statically, and dynamically stable. Furthermore, the designed control surfaces satisfy the critical requirements and are able to adequately follow and react to the input commands. This study carries a great deal of significance for the stability and especially control design engineers working in the domain of UAV design as it presents simple method for developing a complete 6-degree-of-freedom(6-DOF) FDM.\n</div>\n\n\n</div>\n\n\n\n\n\n    </div>\n  </div>\n\n  <div class=\"bibbase_group_whole\" id=\"group_2023\">\n    <div class=\"bibbase_group\"\n      onclick=\"toggleGroup('group_2023')\"\n      onkeypress=\"toggleGroup('group_2023')\"\n      tabindex=\"0\">\n      <i class=\"fa fa-angle-down bibbase_group_head_icon\"></i>&nbsp;\n      <span>2023</span>\n      <span class=\"bibbase_group_count\">\n        \n        (2)\n        \n      </span>\n    </div>\n    <div class=\"bibbase_group_body\">\n      \n  \n  <div class=\"bibbase_paper\" id=\"rauf-khan-alishah-stabilityanalysisdevelopmentofacontrolstrategyforasmalluav-2023\">\n  <span class=\"bibbase_paper_titleauthoryear\">\n\n  \n  <span class=\"bibbase_paper_title\">\n  \n  \n  \n  Stability Analysis & Development of a Control Strategy for a Small UAV.\n  \n  \n  \n</span>\n\n  <span class=\"bibbase_paper_author\">\n  <a class=\"bibbase author link\" href=\"https://maliknaumanrauf.me/publications.html\">Rauf, M. N.</a>; Khan, R. A.;  and Ali Shah, S. I.\n</span>\n\n  \n\n</span>\n\n  In <i>2023 3rd International Conference on Digital Futures and Transformative Technologies (ICoDT2)</i>, pages 1-6,  2023. \n  <span class=\"note\"></span>\n\n<span class=\"bibbase_note\"></span>\n\n<br class=\"bibbase_paper_content\"/>\n\n<span class=\"bibbase_paper_content dontprint\">\n\n  \n\n  \n  <a href=\"http://doi.org/10.1109/ICoDT259378.2023.10325756\"\n     onclick=\"log_download('rauf-khan-alishah-stabilityanalysisdevelopmentofacontrolstrategyforasmalluav-2023', 'http://doi.org/10.1109/ICoDT259378.2023.10325756', event.ctrlKey)\"\n     class=\"bibbase doi link\">\n    <span>doi</span></a>\n  &nbsp;\n  \n\n  \n  <a href=\"//bibbase.org/network/publication/rauf-khan-alishah-stabilityanalysisdevelopmentofacontrolstrategyforasmalluav-2023\"\n     class=\"bibbase bibbase_page link\">link</a>\n  &nbsp;\n  \n\n  <a href=\"#\"\n     onclick=\"showBib(event); return false;\"\n     class=\"bibbase bibtex link\">bibtex\n    <i class=\"fa fa-caret-down\"></i></a>\n\n  \n\n  \n\n  <!-- <a class=\"bibbase read link hidden\" -->\n  <!--    href=\"javascript:toggleRead('rauf-khan-alishah-stabilityanalysisdevelopmentofacontrolstrategyforasmalluav-2023')\" -->\n  <!--    title=\"Marking this paper as read adds it to your library on BibBase.\" -->\n  <!--    > -->\n  <!--   <i class=\"fa fa-check\"></i>&nbsp; -->\n  <!--   <span>mark as read</span> -->\n  <!-- </a> -->\n\n  &nbsp;\n  \n  \n  \n  \n\n</span>\n\n<div class=\"well well-small bibbase\" data-type=\"bibtex\"\n     style=\"display:none\">\n  <pre style=\"white-space: pre-wrap;\">@INPROCEEDINGS{10325756,\r\n\tauthor={Rauf, Malik Nauman and Khan, Roohan Ahmed and Ali Shah, Syed Irtiza},\r\n\tbooktitle={2023 3rd International Conference on Digital Futures and Transformative Technologies (ICoDT2)}, \r\n\ttitle={Stability Analysis &amp; Development of a Control Strategy for a Small UAV}, \r\n\tyear={2023},\r\n\tvolume={},\r\n\tnumber={},\r\n\tpages={1-6},\r\n\tkeywords={Analytical models;Control design;Atmospheric modeling;Autonomous aerial vehicles;Controllability;Stability analysis;Frequency division multiplexing;UAV;Stability;Vortex-lattice Method;Dynamics Modeling;Control Implementation;Feedback Control;LQR},\r\n\tdoi={10.1109/ICoDT259378.2023.10325756}}\r\n\r\n\r\n</pre>\n</div>\n\n\n\n</div>\n\n\n  <div class=\"bibbase_paper\" id=\"rauf-khan-majeed-designingananalysisframeworkforestimatinglifeofacomponentsubjectedtoaconstantloadandasingleoverloadusingmatlab-2023\">\n  <span class=\"bibbase_paper_titleauthoryear\">\n\n  \n  <span class=\"bibbase_paper_title\">\n  \n  \n  \n  <a href=\"https://www.researchgate.net/publication/365903636_Designing_an_Analysis_Framework_for_estimating_life_of_a_component_subjected_to_a_constant_load_and_a_single_overload_using_MATLAB\"\n     onclick=\"return trackOutboundLink('publications', 'click', 'rauf-khan-majeed-designingananalysisframeworkforestimatinglifeofacomponentsubjectedtoaconstantloadandasingleoverloadusingmatlab-2023', 'https://www.researchgate.net/publication/365903636_Designing_an_Analysis_Framework_for_estimating_life_of_a_component_subjected_to_a_constant_load_and_a_single_overload_using_MATLAB', event);\">\n    Designing an Analysis Framework for Estimating Life of a Component Subjected to a Constant Load and a Single Overload Using MATLAB.\n  </a>\n  \n  \n  \n</span>\n\n  <span class=\"bibbase_paper_author\">\n  <a class=\"bibbase author link\" href=\"https://maliknaumanrauf.me/publications.html\">Rauf, M. N.</a>; Khan, R.;  and Majeed, G.\n</span>\n\n  \n\n</span>\n\n  .  2023.\n  <span class=\"note\"></span>\n\n<span class=\"bibbase_note\"></span>\n\n<br class=\"bibbase_paper_content\"/>\n\n<span class=\"bibbase_paper_content dontprint\">\n\n  \n  <a href=\"https://www.researchgate.net/publication/365903636_Designing_an_Analysis_Framework_for_estimating_life_of_a_component_subjected_to_a_constant_load_and_a_single_overload_using_MATLAB\"\n     onclick=\"log_download('rauf-khan-majeed-designingananalysisframeworkforestimatinglifeofacomponentsubjectedtoaconstantloadandasingleoverloadusingmatlab-2023', 'https://www.researchgate.net/publication/365903636_Designing_an_Analysis_Framework_for_estimating_life_of_a_component_subjected_to_a_constant_load_and_a_single_overload_using_MATLAB', event.ctrlKey, event)\">\n    <img src=\"//bibbase.org/img/filetypes/link.svg\"\n\t     alt=\"Designing an Analysis Framework for Estimating Life of a Component Subjected to a Constant Load and a Single Overload Using MATLAB [link]\"\n       title=\"Paper\"\n       style=\"max-height: 1em;\"\n\t     class=\"bibbase_icon\"\n         ><span class=\"bibbase_icon_text\">Paper</span></a>\n  &nbsp;\n  \n\n  \n\n  \n  <a href=\"//bibbase.org/network/publication/rauf-khan-majeed-designingananalysisframeworkforestimatinglifeofacomponentsubjectedtoaconstantloadandasingleoverloadusingmatlab-2023\"\n     class=\"bibbase bibbase_page link\">link</a>\n  &nbsp;\n  \n\n  <a href=\"#\"\n     onclick=\"showBib(event); return false;\"\n     class=\"bibbase bibtex link\">bibtex\n    <i class=\"fa fa-caret-down\"></i></a>\n\n  \n  &nbsp;\n  <a class=\"bibbase_abstract_link bibbase link\"\n     href=\"#\"\n     onclick=\"showAbstract(event); return false;\">\n    abstract <i class=\"fa fa-caret-down\"></i></a>\n  \n\n  \n  &nbsp;\n  <span class=\"bibbase_stats_paper\" style=\"color: #777;\">\n    <span>3 downloads</span>\n  </span>\n  \n\n  <!-- <a class=\"bibbase read link hidden\" -->\n  <!--    href=\"javascript:toggleRead('rauf-khan-majeed-designingananalysisframeworkforestimatinglifeofacomponentsubjectedtoaconstantloadandasingleoverloadusingmatlab-2023')\" -->\n  <!--    title=\"Marking this paper as read adds it to your library on BibBase.\" -->\n  <!--    > -->\n  <!--   <i class=\"fa fa-check\"></i>&nbsp; -->\n  <!--   <span>mark as read</span> -->\n  <!-- </a> -->\n\n  &nbsp;\n  \n  \n  \n  \n  \n  \n  \n  \n  \n  \n  \n  \n\n</span>\n\n<div class=\"well well-small bibbase\" data-type=\"bibtex\"\n     style=\"display:none\">\n  <pre style=\"white-space: pre-wrap;\">@article{Rauf2023,\r\n\tabstract = {Actual Structures are subjected to variable amplitude loading as opposed to a monotone. Many models have been proposed to study these effects analytically. The proposed study focuses on developing an algorithm, and a corresponding framework in MATLAB for two of these models, i.e. the NASGRO equation for constant amplitude loading, and Generalized Willenborg for overload effects. The overload influence is modelled by keeping track of changes in the crack-tip plastic-zone. Two cases are studied with the algorithm, and the results indicate that the presence of overload tends to retard crack growth, thereby validating our algorithm with literature findings.},\r\n\tauthor = {Malik Nauman Rauf and Rahma Khan and Gohar Majeed},\r\n\tkeywords = {Generalized Willenborg,MATLAB,NASGRO,Plastic Zone,Variable Amplitude Loading},\r\n\ttitle = {Designing an Analysis Framework for Estimating Life of a Component Subjected to a Constant Load and a Single Overload Using MATLAB},\r\n\turl = {https://www.researchgate.net/publication/365903636_Designing_an_Analysis_Framework_for_estimating_life_of_a_component_subjected_to_a_constant_load_and_a_single_overload_using_MATLAB},\r\n\tyear = {2023}\r\n}\r\n\r\n\r\n\r\n</pre>\n</div>\n\n\n<div class=\"well well-small bibbase\" data-type=\"abstract\"\n     style=\"display:none\">\n  Actual Structures are subjected to variable amplitude loading as opposed to a monotone. Many models have been proposed to study these effects analytically. The proposed study focuses on developing an algorithm, and a corresponding framework in MATLAB for two of these models, i.e. the NASGRO equation for constant amplitude loading, and Generalized Willenborg for overload effects. The overload influence is modelled by keeping track of changes in the crack-tip plastic-zone. Two cases are studied with the algorithm, and the results indicate that the presence of overload tends to retard crack growth, thereby validating our algorithm with literature findings.\n</div>\n\n\n</div>\n\n\n\n\n\n    </div>\n  </div>\n\n\n\n\n  </div>\n\n\n  <!-- Modal -->\n\n  <!-- <iframe id=\"bibbase_network_frame\" -->\n  <!--         src=\"//bibbase.org/network/control\" -->\n  <!--         style=\"display: none;\"> -->\n  <!-- </iframe> -->\n\n</div>\n"}; document.write(bibbase_data.data);