| 000 |
|
01071nam0 2200277 450 |
| 010 |
__ |
■a978-7-03-044526-1■dCNY89.00 |
| 100 |
__ |
■a20150918d2015 em y0chiy50 ea |
| 101 |
0_ |
■achi |
| 102 |
__ |
■aCN■b110000 |
| 105 |
__ |
■aa a 000yy |
| 106 |
__ |
■ar |
| 200 |
1_ |
■a航天器执行机构姿态容错控制■f张爱华, 霍星著■Ahang tian qi zhi xing ji gou zi t+...... |
| 210 |
__ |
■a北京■c科学出版社■d2015.08 |
| 215 |
__ |
■a211页■c图■d24cm |
| 300 |
__ |
■a并列题名:Actuator attitute fault tolerant control for spacecra+...... |
| 312 |
__ |
■a英文题名取自封面 |
| 320 |
__ |
■a有书目 (第193-211页) |
| 330 |
__ |
■a本书将理论和应用相结合, 分别以过驱动航天器及未配备冗余执行机构的航天器为姿态控制目标, 深入浅出地介绍了航天器执行+...... |
| 510 |
1_ |
■aActuator attitute fault tolerant control for spacecraft■ze+...... |
| 606 |
0_ |
■a航天器■x执行机构■x容错技术■Ahang tian qi |
| 690 |
__ |
■aV448.22■v4 |
| 701 |
_0 |
■a张爱华■4著■Azhang ai hua |
| 701 |
_0 |
■a霍星■4著■Ahuo xing |
| 801 |
_0 |
■aCN■bGSXY■c20170602 |
| 905 |
|
■aGSXY■fV448.22/Z119■g1302821■g1302822 |
| 999 |
__ |
■Mlwq■m20170602 14:36:49 |