Matches in SemOpenAlex for { <https://semopenalex.org/work/W4366153231> ?p ?o ?g. }
Showing items 1 to 76 of
76
with 100 items per page.
- W4366153231 endingPage "48" @default.
- W4366153231 startingPage "43" @default.
- W4366153231 abstract "During its course from a launch site to an intended orbit, a launch vehicle faces an adverse environment and withstand a plethora of disturbances. The set of disturbance forces acting on each stage of the vehicle depends on the configuration of that stage. Different methodologies are used to predict the magnitude of static disturbances before the flight. To ensure the launch success, performance of a flight control system is validated using a high fidelity six degrees of freedom simulation testbed, in the presence of predicted magnitude of these disturbances. Magnitude experienced by the launch vehicle during its maiden flight, might vary from the predicted set. Actual magnitude of these disturbances is known only after the flight in post-flight exercise of matching launch vehicle dynamics using ground simulations. Correct information of the magnitude of these disturbances is of significant importance for subsequent developmental flights. Control power plant sizing, preflight actuator biasing to nullify lift-off disturbance and autopilot integrator limit setting are all dependent on the exact knowledge of these sources of disturbances. Flight data measurements of a launch vehicle offer a rich galore of information in this regard. This paper presents an analytical technique which uses flight measurements to compute static disturbances experienced during the flight by a launch vehicle. The main sources of steady disturbances considered in this paper are center of gravity, thrust-line offset and thrust misalignment." @default.
- W4366153231 created "2023-04-19" @default.
- W4366153231 creator A5003440424 @default.
- W4366153231 creator A5005822202 @default.
- W4366153231 creator A5019974463 @default.
- W4366153231 creator A5068514847 @default.
- W4366153231 creator A5078092280 @default.
- W4366153231 creator A5089920755 @default.
- W4366153231 date "2022-01-01" @default.
- W4366153231 modified "2023-10-14" @default.
- W4366153231 title "Computation of static disturbances experienced by a launch vehicle during the flight" @default.
- W4366153231 cites W1984668387 @default.
- W4366153231 cites W1991507689 @default.
- W4366153231 cites W2498563184 @default.
- W4366153231 doi "https://doi.org/10.1016/j.ifacol.2023.03.008" @default.
- W4366153231 hasPublicationYear "2022" @default.
- W4366153231 type Work @default.
- W4366153231 citedByCount "0" @default.
- W4366153231 crossrefType "journal-article" @default.
- W4366153231 hasAuthorship W4366153231A5003440424 @default.
- W4366153231 hasAuthorship W4366153231A5005822202 @default.
- W4366153231 hasAuthorship W4366153231A5019974463 @default.
- W4366153231 hasAuthorship W4366153231A5068514847 @default.
- W4366153231 hasAuthorship W4366153231A5078092280 @default.
- W4366153231 hasAuthorship W4366153231A5089920755 @default.
- W4366153231 hasBestOaLocation W43661532311 @default.
- W4366153231 hasConcept C114008111 @default.
- W4366153231 hasConcept C121332964 @default.
- W4366153231 hasConcept C126691448 @default.
- W4366153231 hasConcept C127413603 @default.
- W4366153231 hasConcept C1276947 @default.
- W4366153231 hasConcept C13393347 @default.
- W4366153231 hasConcept C146978453 @default.
- W4366153231 hasConcept C154945302 @default.
- W4366153231 hasConcept C206923515 @default.
- W4366153231 hasConcept C2775924081 @default.
- W4366153231 hasConcept C41008148 @default.
- W4366153231 hasConcept C41376638 @default.
- W4366153231 hasConcept C44154836 @default.
- W4366153231 hasConcept C47446073 @default.
- W4366153231 hasConcept C79420006 @default.
- W4366153231 hasConceptScore W4366153231C114008111 @default.
- W4366153231 hasConceptScore W4366153231C121332964 @default.
- W4366153231 hasConceptScore W4366153231C126691448 @default.
- W4366153231 hasConceptScore W4366153231C127413603 @default.
- W4366153231 hasConceptScore W4366153231C1276947 @default.
- W4366153231 hasConceptScore W4366153231C13393347 @default.
- W4366153231 hasConceptScore W4366153231C146978453 @default.
- W4366153231 hasConceptScore W4366153231C154945302 @default.
- W4366153231 hasConceptScore W4366153231C206923515 @default.
- W4366153231 hasConceptScore W4366153231C2775924081 @default.
- W4366153231 hasConceptScore W4366153231C41008148 @default.
- W4366153231 hasConceptScore W4366153231C41376638 @default.
- W4366153231 hasConceptScore W4366153231C44154836 @default.
- W4366153231 hasConceptScore W4366153231C47446073 @default.
- W4366153231 hasConceptScore W4366153231C79420006 @default.
- W4366153231 hasIssue "22" @default.
- W4366153231 hasLocation W43661532311 @default.
- W4366153231 hasOpenAccess W4366153231 @default.
- W4366153231 hasPrimaryLocation W43661532311 @default.
- W4366153231 hasRelatedWork W2005151008 @default.
- W4366153231 hasRelatedWork W2085099727 @default.
- W4366153231 hasRelatedWork W2111125015 @default.
- W4366153231 hasRelatedWork W2275901616 @default.
- W4366153231 hasRelatedWork W2360571364 @default.
- W4366153231 hasRelatedWork W287639772 @default.
- W4366153231 hasRelatedWork W2921596957 @default.
- W4366153231 hasRelatedWork W2993320072 @default.
- W4366153231 hasRelatedWork W3170442224 @default.
- W4366153231 hasRelatedWork W4280643413 @default.
- W4366153231 hasVolume "55" @default.
- W4366153231 isParatext "false" @default.
- W4366153231 isRetracted "false" @default.
- W4366153231 workType "article" @default.