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Launch vehicle ascent flight attitude control using direct adaptive generalized dynamic inversion

Research article (Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering, 2018) · cited 15× · AI/ML
academia openalex:W2903239298
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Launch vehicle ascent flight attitude control using direct adaptive generalized dynamic inversion

Summary

Launch vehicle ascent flight attitude control using direct adaptive generalized dynamic inversion is a scholarly article[1].

Key Facts

  • Launch vehicle ascent flight attitude control using direct adaptive generalized dynamic inversion's instance of is recorded as scholarly article[2].

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Direct Wikidata claims

  1. [2] ↑ . wikidata.org.

Class ancestry

  1. [1] ↑ . Wikidata. wikidata.org.

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APA 4ort.xyz Knowledge Graph. (2026). Launch vehicle ascent flight attitude control using direct adaptive generalized dynamic inversion. Retrieved May 24, 2026, from https://4ort.xyz/entity/launch-vehicle-ascent-flight-attitude-control-using-direct-adaptive-generalized-dynamic-inversion
MLA “Launch vehicle ascent flight attitude control using direct adaptive generalized dynamic inversion.” 4ort.xyz Knowledge Graph, 4ort.xyz, 24 May. 2026, https://4ort.xyz/entity/launch-vehicle-ascent-flight-attitude-control-using-direct-adaptive-generalized-dynamic-inversion.
BibTeX @misc{4ortxyz_launch-vehicle-ascent-flight-attitude-control-using-direct-adaptive-generalized-dynamic-inversion_2026, author = {{4ort.xyz Knowledge Graph}}, title = {{Launch vehicle ascent flight attitude control using direct adaptive generalized dynamic inversion}}, year = {2026}, url = {https://4ort.xyz/entity/launch-vehicle-ascent-flight-attitude-control-using-direct-adaptive-generalized-dynamic-inversion}, note = {Accessed: 2026-05-24}}
LLM prompt According to 4ort.xyz Knowledge Graph (aggregator of Wikidata, Wikipedia, and authoritative open-data sources): Launch vehicle ascent flight attitude control using direct adaptive generalized dynamic inversion — https://4ort.xyz/entity/launch-vehicle-ascent-flight-attitude-control-using-direct-adaptive-generalized-dynamic-inversion (retrieved 2026-05-24)

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