Finite-time output feedback control of spacecraft attitude based on “adding a power integrator” method
2021 ◽
pp. 095441002110177
Keyword(s):
Keyword(s):
Keyword(s):
2020 ◽
Vol 357
(16)
◽
pp. 11421-11447
Keyword(s):
2017 ◽
Vol 354
(15)
◽
pp. 6747-6765
◽
2016 ◽
Vol 90
(7)
◽
pp. 1457-1465
◽
Keyword(s):
2019 ◽
Vol 51
(1)
◽
pp. 87-101
◽
2019 ◽
Vol 17
(11)
◽
pp. 2948-2960
◽
Keyword(s):