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wyszukanych pozycji: 9
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State Estimation and Control for Low-Cost Unmanned Aerial Vehicles
ISBN: 9783319363967 / Angielski / Miękka / 2016 / 232 str. Termin realizacji zamówienia: ok. 16-18 dni roboczych. The performance of different control methods is investigated and the results compared.State Estimation and Control of Low-Cost Unmanned Aerial Vehicles covers all the important issues for designing a guidance, navigation and control (GNC) system of a low-cost UAV.
The performance of different control methods is investigated and the results compared.State Estimation and Control of Low-Cost Unmanned Aerial Vehicle...
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cena:
402,53 |
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State Estimation and Control for Low-Cost Unmanned Aerial Vehicles
ISBN: 9783319164168 / Angielski / Twarda / 2015 / 232 str. Termin realizacji zamówienia: ok. 16-18 dni roboczych. This book discusses state estimation and control procedures for a low-cost unmanned aerial vehicle (UAV). The authors consider the use of robust adaptive Kalman filter algorithms and demonstrate their advantages over the optimal Kalman filter in the context of the difficult and varied environments in which UAVs may be employed. Fault detection and isolation (FDI) and data fusion for UAV air-data systems are also investigated, and control algorithms, including the classical, optimal, and fuzzy controllers, are given for the UAV. The performance of different control methods is investigated and...
This book discusses state estimation and control procedures for a low-cost unmanned aerial vehicle (UAV). The authors consider the use of robust adapt...
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cena:
402,53 |
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Fault Diagnosis and Reconfiguration in Flight Control Systems
ISBN: 9781402076053 / Angielski / Twarda / 2003 / 342 str. Termin realizacji zamówienia: ok. 16-18 dni roboczych. The problem of fault diagnosis and reconfigurable control is a new and actually developing field of science and engineering. The subject becomes more interesting since there is an increasing demand for the navigation and control systems of aerospace vehicles, automated actuators etc. to be more safe and reliable. Nowadays, the problems of fault detection and isolation and reconfigurable control attract the attention the scientists in the world. The subject is emphasized in the recent international congresses such as IF AC World Congresses (San Francisco-1996, Beijing-1999, and Barcelona-2002)...
The problem of fault diagnosis and reconfigurable control is a new and actually developing field of science and engineering. The subject becomes more ...
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cena:
805,10 |
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Kalman Filtering Based Fault Tolerant Integrated INS/Radar Altimeter
ISBN: 9783659362231 / Angielski / Miękka / 2013 / 144 str. Termin realizacji zamówienia: ok. 10-14 dni roboczych. Navigation and guidance of a flight vehicle require that the altitude of the vehicle must be determined accurately. For this purpose different altimeter measurements can be integrated using Kalman filtering. In this monograph, the integrated navigation system, consisting of INS and radar altimeters, is presented. INS and the radar altimeter have different benefits and drawbacks. While having outstanding high frequency characteristics, the INS is a dead-reckoning system, at which the errors accumulate time by time. The radar altimeter, as a stand-alone system, gets timely updated measurements,...
Navigation and guidance of a flight vehicle require that the altitude of the vehicle must be determined accurately. For this purpose different altimet...
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cena:
263,91 |
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Fault Diagnosis and Reconfiguration in Flight Control Systems
ISBN: 9781461348184 / Angielski / Miękka / 2013 / 342 str. Termin realizacji zamówienia: ok. 16-18 dni roboczych. The problem of fault diagnosis and reconfigurable control is a new and actually developing field of science and engineering. The subject becomes more interesting since there is an increasing demand for the navigation and control systems of aerospace vehicles, automated actuators etc. to be more safe and reliable. Nowadays, the problems of fault detection and isolation and reconfigurable control attract the attention the scientists in the world. The subject is emphasized in the recent international congresses such as IF AC World Congresses (San Francisco-1996, Beijing-1999, and Barcelona-2002)...
The problem of fault diagnosis and reconfigurable control is a new and actually developing field of science and engineering. The subject becomes more ...
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cena:
805,10 |
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Intelligent Based Aircraft Engine Health Monitoring
ISBN: 9783845419657 / Angielski / Miękka / 2011 / 132 str. Termin realizacji zamówienia: ok. 10-14 dni roboczych. Engine Health monitoring (EHM) has been very popular subject to increase aircraft availability with the minimum maintenance cost. The study is aimed at providing a method to monitor the aircraft engine health during the flight with the aim of providing an opportunity for early fault detection to improve airline maintenance effectiveness and reliability. Since the impending engine failures may cause to change the engine parameters such as Fuel Flow (FF), Exhaust Gas Temperature (EGT), engine fan speed (N1), engine compressor speed (N2), etc., engine deteriorations or faults may be identified...
Engine Health monitoring (EHM) has been very popular subject to increase aircraft availability with the minimum maintenance cost. The study is aimed a...
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cena:
263,91 |
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Gyroless Attitude Determination of Nanosatellites : Single-Frame Methods and Kalman Filtering Approach
ISBN: 9783330047815 / Angielski / Miękka / 2017 / 196 str. Termin realizacji zamówienia: ok. 10-14 dni roboczych. |
cena:
290,29 |
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Fault Tolerant Attitude Estimation for Small Satellites
ISBN: 9780815369813 / Angielski / Twarda / 2020 / 330 str. Termin realizacji zamówienia: ok. 30 dni roboczych. |
cena:
850,66 |
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Aircraft Icing Detection, Identification and Reconfigurable Control
ISBN: 9783844388749 / Angielski / Miękka / 2011 / 164 str. Termin realizacji zamówienia: ok. 10-14 dni roboczych. This book aims at the detection and identification of airframe icing based on statistical properties of aircraft dynamics and reconfigurable control protecting aircraft from hazardous icing conditions. Icing model of aircraft is represented by five parameters for iced wing airfoils. Icing is detected by a Kalman filtering innovation approach. A neural network structure is embodied such that its inputs are the aircraft estimated measurements, and its outputs are the icing parameters. The necessary training and validation set for the neural network model of the iced aircraft are obtained from...
This book aims at the detection and identification of airframe icing based on statistical properties of aircraft dynamics and reconfigurable control p...
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cena:
304,16 |
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