发文分析
近年国家/地区发文量统计
| 国家/地区 | 数量 |
|---|---|
| USA | 299 |
| CHINA MAINLAND | 166 |
| Italy | 52 |
| Canada | 51 |
| England | 34 |
| GERMANY (FED REP GER) | 34 |
| Netherlands | 32 |
| Israel | 28 |
| South Korea | 25 |
| India | 23 |
近年机构发文量统计
| 机构 | 数量 |
|---|---|
| BEIHANG UNIVERSITY | 50 |
| NATIONAL AERONAUTICS & SPACE ADMINISTRATION (N... | 33 |
| UNITED STATES DEPARTMENT OF DEFENSE | 32 |
| UNIVERSITY OF COLORADO SYSTEM | 32 |
| DELFT UNIVERSITY OF TECHNOLOGY | 28 |
| BEIJING INSTITUTE OF TECHNOLOGY | 25 |
| HARBIN INSTITUTE OF TECHNOLOGY | 24 |
| TECHNION ISRAEL INSTITUTE OF TECHNOLOGY | 24 |
| UNIVERSITY OF TEXAS SYSTEM | 24 |
| UNIVERSITY SYSTEM OF GEORGIA | 23 |
近年文章引用他刊数据
| 文章名称 | 引用次数 |
|---|---|
| Real-Time Optimal Control via Deep Neural Networks: Stud... | 20 |
| Fast Homotopy Method for Asteroid Landing Trajectory Opt... | 16 |
| New Impact Time and Angle Guidance Strategy via Virtual ... | 13 |
| Rotation-Matrix-Based Attitude Tracking for Multiple Fle... | 13 |
| Pseudospectral Convex Optimization for Powered Descent a... | 13 |
| Frequency Responses Identification from Multi-Axis Maneu... | 12 |
| Propellant-Optimal Powered Descent Guidance | 12 |
| Observer-Based Fault-Tolerant Attitude Control for Space... | 11 |
| Optimal Rocket Landing Guidance Using Convex Optimizatio... | 10 |
| Sliding-Mode Impact Time Guidance Law Design for Various... | 10 |
近年被他刊引用数据
| 期刊名称 | 引用次数 |
|---|---|
| J GUID CONTROL DYNAM | 1337 |
| AEROSP SCI TECHNOL | 811 |
| ACTA ASTRONAUT | 756 |
| P I MECH ENG G-J AER | 724 |
| IEEE ACCESS | 556 |
| IEEE T AERO ELEC SYS | 354 |
| ADV SPACE RES | 286 |
| J SPACECRAFT ROCKETS | 206 |
| INT J AEROSPACE ENG | 202 |
| NONLINEAR DYNAM | 180 |