Event-Triggered Policy to Spacecraft Attitude Stabilization With Actuator Output Nonlinearities

E-resources

Peer reviewed

Event-Triggered Policy to Spacecraft Attitude Stabilization With Actuator Output Nonlinearities

Dai, Ming-Zhe; Xiao, Bing; Zhang, Chengxi; Wu, Jin

IEEE transactions on circuits and systems. II, Express briefs, 08/2021, Volume: 68, Issue: 8

Journal Article

This brief investigates event-triggered control for spacecraft attitude stabilization under the influence of actuator output nonlinearities. Under a designed event-triggered policy, the influences of actuators' inherent nonlinearity and network quantized transmission are evaluated under a unified framework. Compared with the previous results, the influences of data transmission and actuators' inherent nonlinearities are uniformly described as the actuator output nonlinearities, and the event-triggered policy reduces the effects of constants commonly introduced into triggering conditions on the final state convergence regions and achieves Zeno-free triggering. Simulations verify theoretical results.

Keep searching

Author

Dai, Ming-Zhe | Xiao, Bing | Zhang, Chengxi | Wu, Jin

Access to the JCR database is permitted only to users from Slovenia. Your current IP address is not on the list of IP addresses with access permission, and authentication with the relevant AAI accout is required.

Year	Impact factor		Edition		Category		Classification
Year	JCR	SNIP	JCR	SNIP	JCR	SNIP	JCR	SNIP

Links to authors' personal bibliographies	Links to information on researchers in the SICRIS system

Source: Personal bibliographies and: SICRIS

Upload image

Shelf entry

Adding material to shelf was successful.

Adding material to shelf failed.

It was not necessary to add the material to the shelf.

Permalink

E-mail

Impact factor

Select the library membership card:

DRS, in which the journal is indexed

Citations

Theme