All Relations between attitudes and area 39 of brodmann-1909

Publication Sentence Publish Date Extraction Date Species
Eduardo Espíndola, Yu Tan. A new angular velocity observer for attitude tracking of spacecraft. ISA transactions. 2022-04-12. PMID:35410767. this paper proposes a new angular velocity observer for attitude tracking of spacecraft based on contraction analysis. 2022-04-12 2023-08-13 Not clear
Lei Zhang, Haijiao Nan, Zhiqi Zhao, Yuan Yua. Adaptive disturbance observer-based dual-loop integral-type fast terminal sliding mode control for micro spacecraft and its gimbal tracking device. ISA transactions. 2022-04-01. PMID:35361485. the attitude dynamics of the micro spacecraft is decomposed into two parts, which are used to design controllers to track the angle and the dummy angular velocity signals, respectively. 2022-04-01 2023-08-13 Not clear
Fawaz W Alsaade, Qijia Yao, Mohammed S Al-Zahrani, Ali S Alzahrani, Hadi Jahanshah. Indirect-Neural-Approximation-Based Fault-Tolerant Integrated Attitude and Position Control of Spacecraft Proximity Operations. Sensors (Basel, Switzerland). vol 22. issue 5. 2022-03-10. PMID:35270873. the proposed controller can ensure the relative attitude, angular velocity, position, and velocity stabilize into the small neighborhoods around the origin. 2022-03-10 2023-08-13 Not clear
Qiang Han, Yongshuai Zhou, Xin Liu, Xianguo Tu. Event-Triggered Finite-Time Attitude Cooperative Control for Multiple Unmanned Aerial Vehicles. Applied bionics and biomechanics. vol 2022. 2022-03-03. PMID:35237345. based on the attitude error and angular velocity error, a novel nonsingular terminal sliding mode surface is proposed for the controller with event-triggered scheme. 2022-03-03 2023-08-13 Not clear
P Chen, M Yu, Z Deng, M Zhang, J Liu, J Fan, C Hu, L T. Rotary table wobble error analysis and correction of a rotating accelerometer gravity gradiometer. The Review of scientific instruments. vol 93. issue 2. 2022-03-02. PMID:35232129. we consider the influence of attitude changes, angular velocity, and angular acceleration caused by the wobble on the specific force, and we describe the error transmission process based on the accelerometer configuration and its measurement principle. 2022-03-02 2023-08-13 Not clear
Kai-Yu Hu, Chunxia Yang, Wenjing Su. Adaptive Sliding Mode Fault Compensation for Sensor Faults of Variable Structure Hypersonic Vehicle. Sensors (Basel, Switzerland). vol 22. issue 4. 2022-02-26. PMID:35214423. first, an hfv nonlinear system considering sensor compound faults, disturbance, and the variable structure parameter is established, which is divided into the attitude angle outer and angular rate inner loops. 2022-02-26 2023-08-13 Not clear
b' Giovanni Lavezzi, Nathan J Stang, Marco Ciarci\\xc3\\xa. START: A Satellite Three Axis Rotation Testbed. Micromachines. vol 13. issue 2. 2022-02-25. PMID:35208290.' the testbed is completed by a pc workstation, to generate and stream the desired angular rates of the wheels, and a motion capture system for attitude determination. 2022-02-25 2023-08-13 Not clear
Pengwei Hu, Panpan Huang, Zhenbing Qiu, Jian Yang, Xin Li. A 3D Attitude Estimation Method Based on Attitude Angular Partial Feedback for Polarization-Based Integrated Navigation System. Sensors (Basel, Switzerland). vol 22. issue 3. 2022-02-15. PMID:35161457. a 3d attitude estimation method based on attitude angular partial feedback for polarization-based integrated navigation system. 2022-02-15 2023-08-13 Not clear
Pengwei Hu, Panpan Huang, Zhenbing Qiu, Jian Yang, Xin Li. A 3D Attitude Estimation Method Based on Attitude Angular Partial Feedback for Polarization-Based Integrated Navigation System. Sensors (Basel, Switzerland). vol 22. issue 3. 2022-02-15. PMID:35161457. to minimize the negative impact of pol in this situation, an attitude angular adaptive partial feedback method is proposed. 2022-02-15 2023-08-13 Not clear
Milad Alipour, Maryam Malekzadeh, Alireza Ariae. Practical fractional-order nonsingular terminal sliding mode control of spacecraft. ISA transactions. 2021-11-12. PMID:34763885. a novel multi-purpose sliding surface is constructed, with the aim of bringing the reaction wheels in to rest after every attitude stabilization maneuver, utilizing the fractional-order difference of the quaternion error and the reaction wheels angular momentum error. 2021-11-12 2023-08-13 Not clear
Qiang Chen, Shuzong Xie, Xiongxiong H. Neural-Network-Based Adaptive Singularity-Free Fixed-Time Attitude Tracking Control for Spacecrafts. IEEE transactions on cybernetics. vol 51. issue 10. 2021-10-13. PMID:33119520. then, an adaptive neural controller is developed to guarantee that the attitude tracking error and angular velocity error can both converge into the neighborhood of the equilibrium within a fixed time. 2021-10-13 2023-08-13 Not clear
Bing Xiao, Shen Yi. Large-Angle Velocity-Free Attitude Tracking Control of Satellites: An Observer-Free Framework. IEEE transactions on cybernetics. vol 51. issue 9. 2021-09-16. PMID:31647456. the challenging problem on the design of a large-angle attitude tracking controller for rigid satellites without angular velocity measurements is investigated in this article. 2021-09-16 2023-08-13 Not clear
Meiling Tao, Xiongxiong He, Shuzong Xie, Qiang Che. RBFNN-Based Singularity-Free Terminal Sliding Mode Control for Uncertain Quadrotor UAVs. Computational intelligence and neuroscience. vol 2021. 2021-08-31. PMID:34456992. finally, the attitude and angular velocity errors are finite-time uniformly ultimately bounded (ftuub), and numerical simulations illustrated the satisfactory performance of the designed control scheme. 2021-08-31 2023-08-13 Not clear
Eduardo Espíndola-López, Yu Tan. Global exponential attitude tracking for spacecraft with gyro bias estimation. ISA transactions. vol 116. 2021-08-16. PMID:33551131. relying on contraction analysis, this paper addresses the global attitude tracking problem of a spacecraft when angular velocity measurements are corrupted by bias. 2021-08-16 2023-08-13 Not clear
Ahmed G Ghallab, Ian R Peterse. Velocity-Free Attitude Control of Quadrotors: A Nonlinear Negative Imaginary Approach. Sensors (Basel, Switzerland). vol 21. issue 7. 2021-04-13. PMID:33808192. in this paper, we propose a new approach to the attitude control of quadrotors, by which angular velocity measurements or a model-based observer reconstructing the angular velocity are not needed. 2021-04-13 2023-08-13 Not clear
Minseok Ok, Sungsuk Ok, Jahng Hyon Par. Estimation of Vehicle Attitude, Acceleration, and Angular Velocity Using Convolutional Neural Network and Dual Extended Kalman Filter. Sensors (Basel, Switzerland). vol 21. issue 4. 2021-03-11. PMID:33670219. estimation of vehicle attitude, acceleration, and angular velocity using convolutional neural network and dual extended kalman filter. 2021-03-11 2023-08-13 Not clear
Neda Navidi, Rene Landr. A New Perspective on Low-Cost MEMS-Based AHRS Determination. Sensors (Basel, Switzerland). vol 21. issue 4. 2021-03-10. PMID:33669466. attitude and heading reference system (ahrs) is the term used to describe a rigid body's angular orientation in three-dimensional space. 2021-03-10 2023-08-13 Not clear
Xianghua Wang, Chee Pin Tan, Fen Wu, Jiandong Wan. Fault-Tolerant Attitude Control for Rigid Spacecraft Without Angular Velocity Measurements. IEEE transactions on cybernetics. vol 51. issue 3. 2021-02-18. PMID:30951486. fault-tolerant attitude control for rigid spacecraft without angular velocity measurements. 2021-02-18 2023-08-13 human
Jijun Geng, Linyuan Xia, Dongjin W. Attitude and Heading Estimation for Indoor Positioning Based on the Adaptive Cubature Kalman Filter. Micromachines. vol 12. issue 1. 2021-02-18. PMID:33451172. accurate attitude and heading estimation based on magnetic, angular rate, and gravity (marg) sensors of micro-electro-mechanical systems (mems) has received increasing attention due to its high availability and independence. 2021-02-18 2023-08-13 human
Jiayi Tian, Neng Xiong, Shifeng Zhang, Huabo Yang, Zhenyu Jian. Integrated guidance and control for missile with narrow field-of-view strapdown seeker. ISA transactions. vol 106. 2020-12-07. PMID:32620367. due to the removal of the mechanically stable platform in the conventional gimbaled seeker, the strapdown seeker's measurement is coupled with the missile body attitude motion, such that the inertial line-of-sight (los) angular rate required to implement traditional guidance laws cannot be measured, and the field-of-view (fov) limit must be considered when designing guidance and control systems for a strapdown homing missile. 2020-12-07 2023-08-13 Not clear