Pub Date : 2023-02-06DOI: 10.1109/JMASS.2023.3242304
Xiangwei Bu;Baoxu Jiang
In this article, a fragility-free prescribed performance control (PPC) approach is proposed for unknown disturbed nonaffine systems with application to flight control of waverider aerocraft (WA). The main improvement is to develop a prescribed funnel containing additional readjusting terms, which is able to autonomously readjust its shape, such that the tracking error, whose value may increase due to parametric perturbations and external disturbances, is always constrained within the prescribed funnel, capable of guaranteeing, for any initial system condition, 1) avoidance of security fragility problem associated with the existing PPC; 2) finite-time prescribed performance concerning tracking errors; and 3) independent of affine model formulation and function approximation. Finally, the addressed design is applied to WA, and compared simulations with practical examples are presented to show the superiority.
{"title":"Fragility-Free Prescribed Performance Control Without Approximation Applied to Waverider Aerocraft","authors":"Xiangwei Bu;Baoxu Jiang","doi":"10.1109/JMASS.2023.3242304","DOIUrl":"https://doi.org/10.1109/JMASS.2023.3242304","url":null,"abstract":"In this article, a fragility-free prescribed performance control (PPC) approach is proposed for unknown disturbed nonaffine systems with application to flight control of waverider aerocraft (WA). The main improvement is to develop a prescribed funnel containing additional readjusting terms, which is able to autonomously readjust its shape, such that the tracking error, whose value may increase due to parametric perturbations and external disturbances, is always constrained within the prescribed funnel, capable of guaranteeing, for any initial system condition, 1) avoidance of security fragility problem associated with the existing PPC; 2) finite-time prescribed performance concerning tracking errors; and 3) independent of affine model formulation and function approximation. Finally, the addressed design is applied to WA, and compared simulations with practical examples are presented to show the superiority.","PeriodicalId":100624,"journal":{"name":"IEEE Journal on Miniaturization for Air and Space Systems","volume":"4 2","pages":"146-156"},"PeriodicalIF":0.0,"publicationDate":"2023-02-06","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"49964188","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2023-02-01DOI: 10.1109/JMASS.2023.3241566
Ao Li;Shuaizheng Liu;Xiaoxiang Hu;Rui Guo
In this article, an improved model predictive static programming (MPSP)-based fault-tolerant control (FTC) scheme is proposed to solve the attitude tracking control problem of the hypersonic vehicle (HSV). In the field of HSV, the MPSP technique has been applied successfully to solve guidance problems of its high computational efficiency. While we try to address the attitude control problem directly using it. The attitude model of HSV with uncertainty and disturbance, together with the fault model of aircraft body injury, is constructed first. The actuator of HSV is suffering from input constraints. Then, a feasible attitude control trajectory is generated by the improved MPSP method. The methodological innovation in this article extends the MPSP technique to the direct control of the attitude of HSV both in the fixed and flexible final time. By utilizing the improved MPSP technique, the complexity of processing multiple constraints and the computation is reduced. The effectiveness of the designed FTC scheme is demonstrated through simulation under different cases with actuator constraints.
{"title":"Fault-Tolerant Attitude Control for Hypersonic Flight Vehicle Subject to Actuators Constraint: A Model Predictive Static Programming Approach","authors":"Ao Li;Shuaizheng Liu;Xiaoxiang Hu;Rui Guo","doi":"10.1109/JMASS.2023.3241566","DOIUrl":"https://doi.org/10.1109/JMASS.2023.3241566","url":null,"abstract":"In this article, an improved model predictive static programming (MPSP)-based fault-tolerant control (FTC) scheme is proposed to solve the attitude tracking control problem of the hypersonic vehicle (HSV). In the field of HSV, the MPSP technique has been applied successfully to solve guidance problems of its high computational efficiency. While we try to address the attitude control problem directly using it. The attitude model of HSV with uncertainty and disturbance, together with the fault model of aircraft body injury, is constructed first. The actuator of HSV is suffering from input constraints. Then, a feasible attitude control trajectory is generated by the improved MPSP method. The methodological innovation in this article extends the MPSP technique to the direct control of the attitude of HSV both in the fixed and flexible final time. By utilizing the improved MPSP technique, the complexity of processing multiple constraints and the computation is reduced. The effectiveness of the designed FTC scheme is demonstrated through simulation under different cases with actuator constraints.","PeriodicalId":100624,"journal":{"name":"IEEE Journal on Miniaturization for Air and Space Systems","volume":"4 2","pages":"136-145"},"PeriodicalIF":0.0,"publicationDate":"2023-02-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"49964189","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2023-01-30DOI: 10.1109/JMASS.2023.3240892
Fraj Hariz;Yassine Bouslimani;Mohsen Ghribi
Nowadays, most of the mobile mapping systems (MMSs) use global navigation satellite system (GNSS)/inertial navigation system positioning technology and 2-D sensors to construct maps, self-localize, and gather environmental information, as well. Several problems can arise with traditional architectures of these systems, especially in situations where the GNSS signal is unavailable or multiple paths are involved, such as reliability issues and poor accuracy. Moreover, their cost of up to U.S. $$ $