| 书目名称 | Stability and Control of Conventional and Unconventional Aerospace Vehicle Configurations |
| 副标题 | A Generic Approach f |
| 编辑 | Bernd Chudoba |
| 视频video | |
| 概述 | Presents a stability and control method named AeroMech, which is capable of sizing the primary control effectors of fixed-wing subsonic to hypersonic designs.Offers a novel and feasible generic method |
| 丛书名称 | Springer Aerospace Technology |
| 图书封面 |  |
| 描述 | .This book introduces a stability and control methodology named .AeroMech., capable of sizing the primary control effectors of fixed wing subsonic to hypersonic designs of conventional and unconventional configuration layout. Control power demands are harmonized with static-, dynamic-, and maneuver stability requirements, while taking the six-degree-of-freedom trim state into account. The stability and control analysis solves the static- and dynamic equations of motion combined with non-linear vortex lattice aerodynamics for analysis. ..The true complexity of addressing subsonic to hypersonic vehicle stability and control during the conceptual design phase is hidden in the objective to develop a generic (vehicle configuration independent) methodology concept. The inclusion of geometrically asymmetric aircraft layouts, in addition to the reasonably well-known symmetric aircraft types, contributes significantly to the overall technical complexity and level of abstraction. The first three chapters describe the preparatory work invested along with the research strategy devised, thereby placing strong emphasis on systematic and thorough knowledge utilization. The engineering-scientific |
| 出版日期 | Book 2019 |
| 关键词 | aircraft conceptual design; control power assessment; sizing control effectors; trimmed aerodynamics; sa |
| 版次 | 1 |
| doi | https://doi.org/10.1007/978-3-030-16856-8 |
| isbn_softcover | 978-3-030-16858-2 |
| isbn_ebook | 978-3-030-16856-8Series ISSN 1869-1730 Series E-ISSN 1869-1749 |
| issn_series | 1869-1730 |
| copyright | Springer Nature Switzerland AG 2019 |
发表于 2025-3-21 19:42:07
