Matches in SemOpenAlex for { <https://semopenalex.org/work/W2809835770> ?p ?o ?g. }
Showing items 1 to 77 of
77
with 100 items per page.
- W2809835770 abstract "This paper introduces a novel methodology in order to recover an agile maneuvering aircraft from upset conditions as swiftly as possible. The current methodology based on an angular rate grid, which consists of angular velocity nodes. The aircraft is said to start its motion from an initial condition while the initial angular velocity corresponds to a certain node within the aforementioned angular rate grid. A nonlinear dynamic inversion (NDI) based controller is employed to reach transition angular rates, which are the desired rates before the recovery initiates. Once the desired transition node is reached, the controller produces necessary input signals to recover the aircraft. The time elapsed throughout the whole recovery process is recorded. The same sequence of control actions are repeated for each initial and transition nodes of the grid. In this way, a recovery time graph is obtained. The time graph is then used to determine the reference angular rate trajectory, which provides the minimum recovery time for the given rate envelope. Simulations are carried out by employing a nonlinear high fidelity F-16 model. Simulation results show that there exist such angular rate trajectories results with faster recovery. Therefore, the aforementioned results point out nonintuitive solutions. That is, for certain initial states it is not suitable to directly regulate the angular rates when recovery time is considered. Rather, for some cases, it is more convenient to increase the roll rate first, and then regulate the angular rates." @default.
- W2809835770 created "2018-07-10" @default.
- W2809835770 creator A5028990507 @default.
- W2809835770 creator A5047866848 @default.
- W2809835770 creator A5047925060 @default.
- W2809835770 date "2018-03-01" @default.
- W2809835770 modified "2023-09-27" @default.
- W2809835770 title "Rate envelope based time efficient strategy for upset recovery of a fighter aircraft" @default.
- W2809835770 cites W1978113443 @default.
- W2809835770 cites W1985287988 @default.
- W2809835770 cites W2166327919 @default.
- W2809835770 cites W2493736175 @default.
- W2809835770 cites W654568086 @default.
- W2809835770 doi "https://doi.org/10.1109/aero.2018.8396500" @default.
- W2809835770 hasPublicationYear "2018" @default.
- W2809835770 type Work @default.
- W2809835770 sameAs 2809835770 @default.
- W2809835770 citedByCount "0" @default.
- W2809835770 crossrefType "proceedings-article" @default.
- W2809835770 hasAuthorship W2809835770A5028990507 @default.
- W2809835770 hasAuthorship W2809835770A5047866848 @default.
- W2809835770 hasAuthorship W2809835770A5047925060 @default.
- W2809835770 hasConcept C121332964 @default.
- W2809835770 hasConcept C127635394 @default.
- W2809835770 hasConcept C1276947 @default.
- W2809835770 hasConcept C13662910 @default.
- W2809835770 hasConcept C154945302 @default.
- W2809835770 hasConcept C158622935 @default.
- W2809835770 hasConcept C190704821 @default.
- W2809835770 hasConcept C2775924081 @default.
- W2809835770 hasConcept C41008148 @default.
- W2809835770 hasConcept C44154836 @default.
- W2809835770 hasConcept C47446073 @default.
- W2809835770 hasConcept C5594486 @default.
- W2809835770 hasConcept C62520636 @default.
- W2809835770 hasConcept C74650414 @default.
- W2809835770 hasConceptScore W2809835770C121332964 @default.
- W2809835770 hasConceptScore W2809835770C127635394 @default.
- W2809835770 hasConceptScore W2809835770C1276947 @default.
- W2809835770 hasConceptScore W2809835770C13662910 @default.
- W2809835770 hasConceptScore W2809835770C154945302 @default.
- W2809835770 hasConceptScore W2809835770C158622935 @default.
- W2809835770 hasConceptScore W2809835770C190704821 @default.
- W2809835770 hasConceptScore W2809835770C2775924081 @default.
- W2809835770 hasConceptScore W2809835770C41008148 @default.
- W2809835770 hasConceptScore W2809835770C44154836 @default.
- W2809835770 hasConceptScore W2809835770C47446073 @default.
- W2809835770 hasConceptScore W2809835770C5594486 @default.
- W2809835770 hasConceptScore W2809835770C62520636 @default.
- W2809835770 hasConceptScore W2809835770C74650414 @default.
- W2809835770 hasLocation W28098357701 @default.
- W2809835770 hasOpenAccess W2809835770 @default.
- W2809835770 hasPrimaryLocation W28098357701 @default.
- W2809835770 hasRelatedWork W1850577750 @default.
- W2809835770 hasRelatedWork W2134279266 @default.
- W2809835770 hasRelatedWork W2157369318 @default.
- W2809835770 hasRelatedWork W2165168528 @default.
- W2809835770 hasRelatedWork W2187678573 @default.
- W2809835770 hasRelatedWork W2317835622 @default.
- W2809835770 hasRelatedWork W2334842502 @default.
- W2809835770 hasRelatedWork W2828218485 @default.
- W2809835770 hasRelatedWork W2886169110 @default.
- W2809835770 hasRelatedWork W2989652932 @default.
- W2809835770 hasRelatedWork W3017071351 @default.
- W2809835770 hasRelatedWork W71827659 @default.
- W2809835770 hasRelatedWork W100080890 @default.
- W2809835770 hasRelatedWork W1780188848 @default.
- W2809835770 hasRelatedWork W2413689482 @default.
- W2809835770 hasRelatedWork W2830288111 @default.
- W2809835770 hasRelatedWork W2848584580 @default.
- W2809835770 hasRelatedWork W298584021 @default.
- W2809835770 hasRelatedWork W3018924320 @default.
- W2809835770 hasRelatedWork W3181596461 @default.
- W2809835770 isParatext "false" @default.
- W2809835770 isRetracted "false" @default.
- W2809835770 magId "2809835770" @default.
- W2809835770 workType "article" @default.