近期，中(zhong)國(guo)(guo)航(hang)天(tian)科技集團有限公司主導制定的國(guo)(guo)際(ji)標準ISO/NP 16615 《衛星(xing)姿態與(yu)軌道控(kong)制系(xi)統穩定運行(xing)要求(qiu)》由(you)國(guo)(guo)際(ji)標準化(hua)組(zu)織（ISO）正式立項。至此，我(wo)國(guo)(guo)主導制定的航(hang)天(tian)領(ling)域國(guo)(guo)際(ji)標準數量增至29項。

衛星姿(zi)(zi)態(tai)(tai)與(yu)軌道(dao)(dao)控(kong)(kong)(kong)制系(xi)(xi)統(tong)簡稱姿(zi)(zi)軌控(kong)(kong)(kong)系(xi)(xi)統(tong)，負(fu)責完(wan)成衛星的姿(zi)(zi)態(tai)(tai)與(yu)軌道(dao)(dao)控(kong)(kong)(kong)制，是保(bao)證衛星基本功能(neng)與(yu)穩定運行的關鍵。ISO/NP 16615《衛星姿(zi)(zi)態(tai)(tai)與(yu)軌道(dao)(dao)控(kong)(kong)(kong)制系(xi)(xi)統(tong)穩定運行要求》根據衛星在軌穩定運行的影響因素，規定了(le)對衛星姿(zi)(zi)態(tai)(tai)與(yu)軌道(dao)(dao)控(kong)(kong)(kong)制系(xi)(xi)統(tong)在軌穩定運行能(neng)力的構(gou)建原(yuan)(yuan)則和要求，包括數據有效性判(pan)斷、異(yi)常(chang)檢測、軟/硬件故障處理、系(xi)(xi)統(tong)級安全邊界、應(ying)急(ji)安全模式等(deng)方面的判(pan)斷原(yuan)(yuan)則和處理要求。同(tong)時(shi)，本標準明(ming)確(que)了(le)星上自主判(pan)斷處理和地面運行維護的功能(neng)界面，以確(que)保(bao)衛星按(an)預期姿(zi)(zi)態(tai)(tai)和軌道(dao)(dao)飛行。（科軒(xuan)）