會議論文
| 學年 | 80 |
|---|---|
| 學期 | 1 |
| 發表日期 | 1992-01-01 |
| 作品名稱 | Optimal ascent to GEO using laser propulsion system |
| 作品名稱（其他語言） | |
| 著者 | Chern, J. S.; Hong, Z. C.; Chang, C. Y.; Chern, W. L. |
| 作品所屬單位 | 淡江大學機械與機電工程學系 |
| 出版者 | |
| 會議名稱 | 43rd Congress of the International Astronautical Federation |
| 會議地點 | Washington D.C., USA |
| 摘要 | The parameter optimization method is used to solve the optimal trajectory for vertical ascent to the GEO with dynamic pressure and thrust acceleration constraints. The time derivative of the velocity magnitude of the vehicle is assumed to be a polynomial function of the flight time, with the coefficients as free parameters to be selected. The required thrust magnitude and angle are derived as functions of the state variables and the polynomial. A first order polynomial function is adopted for numerical computation. The flight time and the two coefficients are selected such that the final condition for GEO insertion is satisfied and the final mass is maximized. With thrust acceleration constraints, it is found that the final mass remaining is 0.1165, 3.414, 10.53, 18.48, and 25.90 percent, respectively. For a vertically ascending trajectory, the relative speed of the vehicle with respect to the atmosphere is the vertical component of the inertial vehicle velocity. |
| 關鍵字 | |
| 語言 | en |
| 收錄於 | |
| 會議性質 | 國際 |
| 校內研討會地點 | |
| 研討會時間 | 19920101~19920101 |
| 通訊作者 | |
| 國別 | USA |
| 公開徵稿 | Y |
| 出版型式 | 紙本 |
| 出處 | 43rd Congress of the International Astronautical Federation, |
| 相關連結 |
機構典藏連結 ( http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/70742 ) |