標(biāo)題: Titlebook: 2023 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2023) Proceedings; Volume II Song Fu Conference proceedings 2024 [打印本頁(yè)] 作者: 力學(xué) 時(shí)間: 2025-3-21 16:17
書目名稱2023 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2023) Proceedings影響因子(影響力)
書目名稱2023 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2023) Proceedings影響因子(影響力)學(xué)科排名
書目名稱2023 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2023) Proceedings網(wǎng)絡(luò)公開度
書目名稱2023 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2023) Proceedings網(wǎng)絡(luò)公開度學(xué)科排名
書目名稱2023 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2023) Proceedings被引頻次
書目名稱2023 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2023) Proceedings被引頻次學(xué)科排名
書目名稱2023 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2023) Proceedings年度引用
書目名稱2023 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2023) Proceedings年度引用學(xué)科排名
書目名稱2023 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2023) Proceedings讀者反饋
書目名稱2023 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2023) Proceedings讀者反饋學(xué)科排名
作者: Tailor 時(shí)間: 2025-3-21 22:54 作者: 審問 時(shí)間: 2025-3-22 01:31 作者: synovial-joint 時(shí)間: 2025-3-22 07:12
External Information Aided Urban Target Tracking with UAVs, to displace that of Feldberg (1969) or my first edition of 1981. My aim is to explain the subject clearly and simply. The electrochemist (or student) who occasionally needs to simulate a diffusion problem numerically but does not wish to go in for sophisticated methods, can make do with the first four chapte978-3-662-02549-9作者: Fecundity 時(shí)間: 2025-3-22 10:10
Effect of High Temperature Steam Inhalation on Aeroengine Performance, digital sphere, shaped by the interplay between digital capitalism and resistance movements. In light of grassroots initiatives advanced by cyber-activists, e-makers and hackers, the book unveils the socio-political and cultural underpinnings of the revolution produced by the digital social innovat作者: 小樣他閑聊 時(shí)間: 2025-3-22 14:49
Challenges for Integration of Drone into National Airspace System,comes (see Delamont, 2000). Whilst implicated in many of these issues, ‘technology’ has simply not merited any particular foregrounding within such accounts.. Yet whereas the ‘new’ information technologies of the 1980s and 1990s could be said in the hindsight to have been little more than tokenistic作者: 描述 時(shí)間: 2025-3-22 19:42 作者: Gingivitis 時(shí)間: 2025-3-22 21:51 作者: Horizon 時(shí)間: 2025-3-23 02:57
Research on Longitudinal Attitude and Velocity Coordinated Control Method for a Low Aspect Ratio Fldological base is being formed and refined. At present, the effect of chains at the level of individual industries, and the impact national and regional conventions and innovations have on them, are being studied; furthermore, a mechanism for implementing strategic changes in those companies that bo作者: 濃縮 時(shí)間: 2025-3-23 09:03 作者: acquisition 時(shí)間: 2025-3-23 09:44 作者: Precursor 時(shí)間: 2025-3-23 17:26 作者: Diatribe 時(shí)間: 2025-3-23 18:49 作者: arboretum 時(shí)間: 2025-3-23 23:38 作者: Moderate 時(shí)間: 2025-3-24 02:31 作者: modish 時(shí)間: 2025-3-24 08:19 作者: Predigest 時(shí)間: 2025-3-24 12:52 作者: Ornithologist 時(shí)間: 2025-3-24 18:00 作者: Affirm 時(shí)間: 2025-3-24 20:10
Disturbance Rejection Control of Morphing Aircraft Based on RBF Neural Networks,ten and covers many of the aspects of DSP with FPGAs. I run a business that specializes exclusively in high performance DSP designs using FPGAs. This book pretty much covers it all, in fact it closely parallels978-3-662-04613-5作者: 盡責(zé) 時(shí)間: 2025-3-25 02:55 作者: COKE 時(shí)間: 2025-3-25 06:08 作者: 在前面 時(shí)間: 2025-3-25 11:29
Performance Analysis of Turbine-Powered Air Circulation System,e battlefield of online commerce, strategy blends with tactics.?.Indeed, the distinction between pure play and hybrid is increasingly redundant as more holistic business models begin to emerge. Digital Stractic978-1-137-57483-1作者: insomnia 時(shí)間: 2025-3-25 13:05
Olivier Blazy,Céline Chevalier,Paul Germouty RBF neural network, uncertain disturbances caused by the deformation are estimated. Compared with the traditional extended state observer, the RBF neural network adaptive algorithm has strong robustness, which can solve the chattering problem caused by wing transition process. A differential auxili作者: anesthesia 時(shí)間: 2025-3-25 19:45 作者: 聯(lián)想記憶 時(shí)間: 2025-3-25 22:19 作者: Gullible 時(shí)間: 2025-3-26 02:38 作者: 豪華 時(shí)間: 2025-3-26 04:32
Asl? Bay,O?uzhan Ersoy,Ferhat Karako?vacy protection. Finally, considering these challenges and successful experiences of manned-aircraft in national airspace, suggestions are proposed from perspective of design, management and operation. Hence, studying the challenges of drone integration into national airspace system could promote de作者: 過于平凡 時(shí)間: 2025-3-26 12:13 作者: Harbor 時(shí)間: 2025-3-26 14:09 作者: 袖章 時(shí)間: 2025-3-26 17:38
When Are Fuzzy Extractors Possible? slope of the pitching moment curve will be. The pressure and streamline distribution on the trailing edge of an airfoil are important reasons for the difference on different scales. Along with the increase of the scale of WIG craft model, the effect of increasing lift and reducing drag brought by g作者: 壯麗的去 時(shí)間: 2025-3-26 23:13 作者: peritonitis 時(shí)間: 2025-3-27 04:35
Advances in Cryptology – ASIACRYPT 2016of the genetic algorithm. On the premise of the pressure ratios of the two VCEs’ compression components are almost the same, due to the CDFS on the high-pressure spool, the high-pressure spool rotational speed (.) of VCE with CDFS is 6800r/min and the . of VCE with VFS is 8000?r/min. Compared to the作者: 推測(cè) 時(shí)間: 2025-3-27 07:50
Advances in Cryptology – ASIACRYPT 2017tegration was used to design and compare Variable Cycle Engine, Adaptive Cycle Engine and mixed flow turbofan engine. The results indicated that “ACE-3Stream 1?+?2” and “ACE-3Bypass M3” have dual advantages in steady-state performance and aerodynamic stability within the flight envelope, achieving h作者: 釘牢 時(shí)間: 2025-3-27 13:20 作者: crutch 時(shí)間: 2025-3-27 15:23
Lecture Notes in Computer Scienceicle. Firstly, the expected attitude and airspeed are calculated based on the desired flight trim conditions, and a speed control method based on INDI theory is presented. Secondly, according to the dynamic constraints, the attitude control law based on the INDI method is designed. To verify the eff作者: wreathe 時(shí)間: 2025-3-27 18:09 作者: 吞沒 時(shí)間: 2025-3-28 00:32 作者: 無(wú)所不知 時(shí)間: 2025-3-28 03:30
Front Matterred many years ago. Indeed, the problem of acoustic echo control is crucial for the design of audio terminals operating in hands-free mode such as hands-free telephone sets, teleconference systems, videoconferencing devices…. The acoustic echo control can be performed by more or less elaborate devic作者: AWE 時(shí)間: 2025-3-28 08:33 作者: assent 時(shí)間: 2025-3-28 11:51
Investigation of Flow Field and Performance of Tandem Flapping Wing Micro Air Vehicle,ling, in the main, with the combinational and sequential logic aspects of system design. By comparison, the coverage of digital hardware has been meagre: in particular, books on logic circuit interconnections have been scarce in number. When circuits operated at relatively low speeds this did not ca作者: FLAG 時(shí)間: 2025-3-28 15:36 作者: 搖曳的微光 時(shí)間: 2025-3-28 21:52 作者: Bmd955 時(shí)間: 2025-3-29 01:57 作者: 轎車 時(shí)間: 2025-3-29 04:22 作者: TRAWL 時(shí)間: 2025-3-29 08:40 作者: 使混合 時(shí)間: 2025-3-29 15:26
Assessment of Modulated Pre-swirl System in the Turbofan Engine by a Multi-dimensional Coupled Modecommunication technology.Spells out the 1st- and 2nd-order cThis book acts as a valuable quick-access resource on the challenges and opportunities that the digital age presents to organizational leadership. Balanced, comprehensive, and thought-provoking, the book will be useful to professionals and 作者: Coma704 時(shí)間: 2025-3-29 16:18
A Method of MCT Determination for Civil Aircraft Based on Scenario Analysis,evious chapter the functional transformation method (FTM) first subdivides the musical instrument into different parts that are analyzed independently from each other as described in section 2. In contrast to the DWG and the MS, the FTM does not approximate the resulting sound or measured vibrationa作者: AROMA 時(shí)間: 2025-3-29 22:50
Research on Data Reconstruction Methods Based on Multiple Models of Aero-Engine Sensor,hichte und die verschiedenen heutigen Auspr?gungen gegeben. Dabei liegt der Fokus auf Digital Storytelling im Web auf Basis von Animation.?.Besonders die Idee der scroll-activated animation als zeitgem??es Konzept für das Storytelling wird in diesem Buch in den Mittelpunkt gestellt.?.Als technische 作者: exclusice 時(shí)間: 2025-3-30 02:49 作者: Nausea 時(shí)間: 2025-3-30 05:01
Research on Longitudinal Attitude and Velocity Coordinated Control Method for a Low Aspect Ratio Flst all countries—whether a developed or developing state—participate in a GVC, regardless of their stage of development. At present, relations in the international trade system are being transformed, and GVCs play a key role in this new world economy; approaches to new product developments, and the 作者: Foreknowledge 時(shí)間: 2025-3-30 09:12
Steady-State Performance Model Identification Method of Low Bypass Ratio Turbofan Engine Based on Eceutical or biotechnology companies, developed through a series of clinical trials, manufactured and finally marketed and sold. In reality, the pharmaceutical value chain is indeed fraught with complications. For example, the main customer of a pharmaceutical sales representative is the physician wh作者: 異常 時(shí)間: 2025-3-30 15:47 作者: VOK 時(shí)間: 2025-3-30 17:07
Conference proceedings 2024sium is a common endeavour among the four national aerospace societies in China, Australia, Korea and Japan, namely, Chinese Society of Aeronautics and Astronautics (CSAA), Royal Aeronautical Society Australian Division (RAeS Australian Division), Japan Society for Aeronautical and Space Sciences (J作者: 不利 時(shí)間: 2025-3-30 23:44 作者: 高度 時(shí)間: 2025-3-31 01:57 作者: 可憎 時(shí)間: 2025-3-31 08:23 作者: 防止 時(shí)間: 2025-3-31 11:16 作者: 流浪 時(shí)間: 2025-3-31 17:21 作者: 機(jī)械 時(shí)間: 2025-3-31 19:35 作者: 一大塊 時(shí)間: 2025-3-31 22:18 作者: lesion 時(shí)間: 2025-4-1 04:40 作者: enmesh 時(shí)間: 2025-4-1 06:50
978-981-97-4012-3The Editor(s) (if applicable) and The Author(s), under exclusive license to Springer Nature Singapor作者: Pcos971 時(shí)間: 2025-4-1 13:57 作者: Ondines-curse 時(shí)間: 2025-4-1 16:55
https://doi.org/10.1007/978-3-662-53890-6try (PIV) measurements were carried out with the variation in the phase difference between fore and hind wings .. We have self-developed a tandem flapping wing drone whose phase difference could be changed every 30°. This drone was used to measure the thrust force and flow field in 48 different cond作者: 多樣 時(shí)間: 2025-4-1 20:51
https://doi.org/10.1007/978-3-662-53890-6d 3D representation, consisting of basic elements such as bricks, cylinders, and spheres, in contrast to the real-world depth map extracted from the environment. Nonetheless, when the object possesses minimal depth, detection becomes unachievable, resulting in a visual output that doesn‘t completely作者: Optometrist 時(shí)間: 2025-4-2 00:28
