標題: Titlebook: Advances in Small Satellite Technologies; Proceedings of 1st I PSR Srinivasa Sastry,Jiji CV,Samba Siva Rao Conference proceedings 2020 Spri [打印本頁] 作者: Coarctation 時間: 2025-3-21 16:40
書目名稱Advances in Small Satellite Technologies影響因子(影響力)
書目名稱Advances in Small Satellite Technologies影響因子(影響力)學科排名
書目名稱Advances in Small Satellite Technologies網(wǎng)絡公開度
書目名稱Advances in Small Satellite Technologies網(wǎng)絡公開度學科排名
書目名稱Advances in Small Satellite Technologies被引頻次
書目名稱Advances in Small Satellite Technologies被引頻次學科排名
書目名稱Advances in Small Satellite Technologies年度引用
書目名稱Advances in Small Satellite Technologies年度引用學科排名
書目名稱Advances in Small Satellite Technologies讀者反饋
書目名稱Advances in Small Satellite Technologies讀者反饋學科排名
作者: falsehood 時間: 2025-3-21 21:33 作者: STANT 時間: 2025-3-22 00:33 作者: LAPSE 時間: 2025-3-22 06:51
De-Tumbling Controller of NIUSAT: Design, Simulation and On-Orbit Performancet it takes reasonable measures to effectively reduce the tumbling of the satellite in a reasonable time. In this paper, we will describe the design details of the de-tumbling controller, digital simulation results and the on-orbit performance on board the NIUSAT nano-satellite.作者: ACE-inhibitor 時間: 2025-3-22 10:12
Optimal Nonlinear Dynamic Inversion-Based Flight Control System Design for an Aerospace Vehiclell as optimal dynamic inversion (ODI). Nonlinear dynamic inversion is the control synthesis technique in which the inherent dynamics of a dynamical system are cancelled out and replaced by desired performance parameters which are selected by the designer. Two-loop control structure is adopted based 作者: Classify 時間: 2025-3-22 16:21 作者: 躲債 時間: 2025-3-22 17:12
Slew Rate and Control Constrained Spacecraft Attitude Maneuver with Reaction Wheel Failurey diagonal and (c) skew configuration with skew angle of 45°, are studied. The paper further discusses single reaction wheel failure conditions for all the three configurations and demonstrates satellite rest to rest maneuver within the slew rate and actuator limits.作者: 虛情假意 時間: 2025-3-22 21:14 作者: Militia 時間: 2025-3-23 02:16 作者: LUT 時間: 2025-3-23 07:19 作者: interlude 時間: 2025-3-23 11:34 作者: 可用 時間: 2025-3-23 17:13 作者: transient-pain 時間: 2025-3-23 19:57
Office Computing and the Right to Privacyd station. In the global scenario, the evolution of Tracking and Data Relay Satellite System (TDRSS) is developed by NASA to support communications and tracking services for its LEO spacecraft. The modern space technologies with low-cost microelectronics and microelectromechanical systems (MEMS) tec作者: diabetes 時間: 2025-3-23 22:40 作者: 延期 時間: 2025-3-24 03:13
PSR Srinivasa Sastry,Jiji CV,Samba Siva RaoDiscusses design and development of cost effective satellite systems.Discusses applications for scientific, operational, public and commercial services.Describes utilization of small satellites for co作者: infinite 時間: 2025-3-24 09:09 作者: excursion 時間: 2025-3-24 11:22 作者: 脆弱么 時間: 2025-3-24 14:54 作者: 藕床生厭倦 時間: 2025-3-24 20:47
Conference proceedings 2020ents relating to small satellite technology. The papers cover various issues relating to design and engineering, ranging from the control, mechanical and thermal systems to the sensors, antennas and RF systems used. The volume will be of interest to scientists and engineers working on or utilizing satellite and space technologies.?.作者: Bouquet 時間: 2025-3-24 23:49 作者: 手榴彈 時間: 2025-3-25 07:05
https://doi.org/10.1007/978-1-4020-4387-1ost, low weight and high reliability. However, piezoelectric transducers are prone to aging effects that cannot be compensated and hence affect gyro drift and scale factor stability. In this paper, two methods of using same piezoelectric transducer element for actuation and sensing are designed and 作者: Suppository 時間: 2025-3-25 11:10 作者: 明智的人 時間: 2025-3-25 13:11
Developments at the Man-Machine Interface,the tethered system is dominated by the tether oscillations and the three-dimensional attitude dynamics of the sub-satellite. The dynamic characters of the system are investigated, and probable control strategies that can be adopted for the faithful and hassle-free deployment of the tether are discu作者: Judicious 時間: 2025-3-25 19:08 作者: 新義 時間: 2025-3-25 21:11 作者: 賭博 時間: 2025-3-26 01:45 作者: 滋養(yǎng) 時間: 2025-3-26 06:08
Problems with System Implementationnlinear system, the linear control design may not be effective as well as does lead to large operational domains. Once the number of operating points increases, gain scheduling process in linear control technique becomes cumbersome. To overcome the demerits of linear control design techniques, the n作者: ANNUL 時間: 2025-3-26 10:11 作者: 黑豹 時間: 2025-3-26 16:29
Office Computing and the Right to Privacy sensing, science, and human in space program. The visibility of the low Earth orbit (LEO) to the ground station is limited for a maximum of ~20?min, with four to five orbital visibilities over a day. This requires a huge network of ground stations. About two-third coverage of the orbit of LEO satel作者: 歡騰 時間: 2025-3-26 19:50 作者: 煉油廠 時間: 2025-3-26 23:51
Silvia Melitta Mueller,Wolfgang J. Paul a desirable characteristic for any mission design. At the same time, a higher slew rate demands a higher actuator torque capacity which is always constrained due to the physical limits of the actuator. This paper discusses the satellite attitude maneuver problem under slew rate and actuator capacit作者: Negotiate 時間: 2025-3-27 03:49 作者: 場所 時間: 2025-3-27 07:24
An Assessment of the MU5 Computer System,quirements of the SAR payload are spelled out, and in turn how we convert those requirements to design of orbit is discussed. The constraints of SAR payload imaging over normal electro-optical payload will be detailed. Mission requirements and payload constraints are converted into specific orbital 作者: Dorsal 時間: 2025-3-27 10:05
I. Karlowsky,H.-O. Leilich,H. Ch. Zeidler bands. This plethora of spectral information enables the detection of targets concealed by tree canopy of camouflage net. This problem cannot be addressed using high-resolution visible data alone because ‘shape information’ provided by such imagery cannot be used reliably in case of concealed targe作者: 充滿裝飾 時間: 2025-3-27 17:36 作者: ASSET 時間: 2025-3-27 19:34 作者: 燦爛 時間: 2025-3-27 22:04
https://doi.org/10.1007/978-1-4020-4387-1ost, low weight and high reliability. However, piezoelectric transducers are prone to aging effects that cannot be compensated and hence affect gyro drift and scale factor stability. In this paper, two methods of using same piezoelectric transducer element for actuation and sensing are designed and evaluated for improving gyro performance.作者: 多嘴 時間: 2025-3-28 02:06
Patient/Parent/Family Educational Assistsntage of the proposed minimal configuration is better for small satellite using off-the-shelf component. There is clear advantage to spin up and spin down of the wheel in this configuration. Attitude determination is now simpler and reliable for the payload pointing to earth or solar panel tracking the sun when the pitch is held to orbit normal.作者: 反叛者 時間: 2025-3-28 07:03 作者: 失眠癥 時間: 2025-3-28 12:29 作者: TIA742 時間: 2025-3-28 16:46
2195-4356 al services.Describes utilization of small satellites for co.This volume contains select papers presented during the?1st International Conference on Small Satellites, discussing the latest research and developments relating to small satellite technology. The papers cover various issues relating to d作者: MUTED 時間: 2025-3-28 21:49
Office Computing and the Right to Privacyd. A detailed description of each of the blocks in CLS framework has been provided. The problems faced due to actuation with magnetorquer are described. It also contains the description of practices followed to ensure the quality (correctness of results obtained and repeatability of the process).作者: 濃縮 時間: 2025-3-29 01:09
Problem-/Language-Orientated Architecture,ts performance for different dual-pol combinations has been assessed. The proposed technique is independent of polarization combinations. Impact on classification when only 50% pixel is considered for selecting initial seed point is demonstrated. RISAT-1 quad-polarimetric data has been used for validating our result.作者: 精美食品 時間: 2025-3-29 06:02 作者: 發(fā)展 時間: 2025-3-29 09:07
Closed-Loop Simulation for Attitude Control of Nano-satellited. A detailed description of each of the blocks in CLS framework has been provided. The problems faced due to actuation with magnetorquer are described. It also contains the description of practices followed to ensure the quality (correctness of results obtained and repeatability of the process).作者: Dappled 時間: 2025-3-29 11:26 作者: 完成才會征服 時間: 2025-3-29 16:19 作者: intellect 時間: 2025-3-29 21:31
Patient/Parent/Family Educational Assistsable for manual testing, automated testing, open-loop bench test, closed-loop attitude control testing and hardware-in-the-loop tests. The test system has been built as a generic tool making the system configurable for any satellite with ease.作者: 玩忽職守 時間: 2025-3-30 00:31
The Configurable Attitude Sensor and Actuator Simulation in the RSAT Test Systemable for manual testing, automated testing, open-loop bench test, closed-loop attitude control testing and hardware-in-the-loop tests. The test system has been built as a generic tool making the system configurable for any satellite with ease.作者: 有說服力 時間: 2025-3-30 07:33
Conference proceedings 2020ents relating to small satellite technology. The papers cover various issues relating to design and engineering, ranging from the control, mechanical and thermal systems to the sensors, antennas and RF systems used. The volume will be of interest to scientists and engineers working on or utilizing s作者: erythema 時間: 2025-3-30 09:31
Developments at the Man-Machine Interface,ssed. Tether is proposed to be released with an initial velocity with constant deceleration using tension in tether. Dynamics of a short tether of 10?m length connected to a 10?kg 3U sub-satellite is considered in the study. Deployment with tether in tension and without tension in tether is discussed.作者: 小樣他閑聊 時間: 2025-3-30 15:42 作者: 摘要 時間: 2025-3-30 20:14
I. Karlowsky,H.-O. Leilich,H. Ch. Zeidlerts. Hence, this problem is modeled as a target detection problem using ‘spectral information’ present in hyperspectral imagery. Moreover, the presence of concealing material such as canopy or cam net over the target necessitates the use of ‘sub-pixel’ target detectors.作者: Decline 時間: 2025-3-30 22:05 作者: Ejaculate 時間: 2025-3-31 03:02
SAR Payload Remote Sensing Satellite Mission Analysis for Global Coverageparameters. SAR payload geometry is discussed, and off-nadir angle, repeat cycle and revisit time relation is detailed. The superiority of the selected orbit is simulated and detailed in the paper. Global coverage analysis studies are simulated and presented.作者: Cleave 時間: 2025-3-31 05:53
Detection of Camouflaged Targets in Hyperspectral Imagests. Hence, this problem is modeled as a target detection problem using ‘spectral information’ present in hyperspectral imagery. Moreover, the presence of concealing material such as canopy or cam net over the target necessitates the use of ‘sub-pixel’ target detectors.作者: HAWK 時間: 2025-3-31 09:27
