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Anti-disturbance autopilot design for missile system via finite time integral sliding mode control method and nonlinear disturbance observer technique
Research article (Transactions of the Institute of Measurement and Control, 2015) · cited 21× · AI/ML
Anti-disturbance autopilot design for missile system via finite time integral sliding mode control method and nonlinear disturbance observer technique
Summary
Anti-disturbance autopilot design for missile system via finite time integral sliding mode control method and nonlinear disturbance observer technique is a scholarly article[1].
Key Facts
Anti-disturbance autopilot design for missile system via finite time integral sliding mode control method and nonlinear disturbance observer technique's instance of is recorded as scholarly article[2].
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APA4ort.xyz Knowledge Graph. (2026). Anti-disturbance autopilot design for missile system via finite time integral sliding mode control method and nonlinear disturbance observer technique. Retrieved May 24, 2026, from https://4ort.xyz/entity/anti-disturbance-autopilot-design-for-missile-system-via-finite-time-integral-sliding-mode-control-method-and-nonlinear-
MLA“Anti-disturbance autopilot design for missile system via finite time integral sliding mode control method and nonlinear disturbance observer technique.” 4ort.xyz Knowledge Graph, 4ort.xyz, 24 May. 2026, https://4ort.xyz/entity/anti-disturbance-autopilot-design-for-missile-system-via-finite-time-integral-sliding-mode-control-method-and-nonlinear-.
BibTeX@misc{4ortxyz_anti-disturbance-autopilot-design-for-missile-system-via-finite-time-integral-sliding-mode-control-method-and-nonlinear-_2026, author = {{4ort.xyz Knowledge Graph}}, title = {{Anti-disturbance autopilot design for missile system via finite time integral sliding mode control method and nonlinear disturbance observer technique}}, year = {2026}, url = {https://4ort.xyz/entity/anti-disturbance-autopilot-design-for-missile-system-via-finite-time-integral-sliding-mode-control-method-and-nonlinear-}, note = {Accessed: 2026-05-24}}
LLM promptAccording to 4ort.xyz Knowledge Graph (aggregator of Wikidata, Wikipedia, and authoritative open-data sources): Anti-disturbance autopilot design for missile system via finite time integral sliding mode control method and nonlinear disturbance observer technique — https://4ort.xyz/entity/anti-disturbance-autopilot-design-for-missile-system-via-finite-time-integral-sliding-mode-control-method-and-nonlinear- (retrieved 2026-05-24)
