Gain Scheduled Finite Horizon LQR for Approach and Landing Phase of a Reusable Launch Vehicle (Record no. 17698)
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| 000 -LEADER | |
|---|---|
| fixed length control field | a |
| 003 - CONTROL NUMBER IDENTIFIER | |
| control field | OSt |
| 005 - DATE AND TIME OF LATEST TRANSACTION | |
| control field | 20220929144545.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION | |
| fixed length control field | 220929b xxu||||| |||| 00| 0 eng d |
| 040 ## - CATALOGING SOURCE | |
| Original cataloging agency | AIKTC-KRRC |
| Transcribing agency | AIKTC-KRRC |
| 100 ## - MAIN ENTRY--PERSONAL NAME | |
| 9 (RLIN) | 18176 |
| Author | Hameed, A. S |
| 245 ## - TITLE STATEMENT | |
| Title | Gain Scheduled Finite Horizon LQR for Approach and Landing Phase of a Reusable Launch Vehicle |
| 250 ## - EDITION STATEMENT | |
| Volume, Issue number | Vol, 103(3), June |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. | |
| Place of publication, distribution, etc. | Kolkatta |
| Name of publisher, distributor, etc. | Springer |
| Year | 2022 |
| 300 ## - PHYSICAL DESCRIPTION | |
| Pagination | 381–388p |
| 520 ## - SUMMARY, ETC. | |
| Summary, etc. | major challenge during the descent of a reusable launch vehicle is to guide the unpowered vehicle to the runway safely by gliding through various phases, of which the third and final phase is Approach and Landing. Several constraints need to be satisfied during this phase in order to accomplish safe landing on the runway within a specified downrange. This paper proposes a simple integrated guidance and control scheme for Approach and Landing based on finite horizon LQR along with gain scheduling in order to achieve the touchdown requirements. A closed loop control law is designed to minimize the errors on the longitudinal vehicle states throughout the two-segment trajectory under off-nominal initial conditions. Simulation results validate that besides satisfying the constraints at touchdown, the scheme is robust enough to handle drag variations existing through out the entire Approach and Landing phase. |
| 650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| 9 (RLIN) | 4626 |
| Topical term or geographic name entry element | Mechanical Engineering |
| 700 ## - ADDED ENTRY--PERSONAL NAME | |
| 9 (RLIN) | 18177 |
| Co-Author | Bindu, G. R |
| 773 0# - HOST ITEM ENTRY | |
| International Standard Serial Number | 2250-0545 |
| Place, publisher, and date of publication | Kolkata Institution of Engineers (India) |
| Title | Journal of the institution of engineers (India): Series C |
| 856 ## - ELECTRONIC LOCATION AND ACCESS | |
| URL | https://link.springer.com/article/10.1007/s40032-021-00789-2 |
| Link text | Click here |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) | |
| Source of classification or shelving scheme | Dewey Decimal Classification |
| Koha item type | Articles Abstract Database |
| Withdrawn status | Lost status | Source of classification or shelving scheme | Damaged status | Not for loan | Home library | Current library | Shelving location | Date acquired | Total Checkouts | Barcode | Date last seen | Price effective from | Koha item type |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Dewey Decimal Classification | School of Engineering & Technology | School of Engineering & Technology | Archieval Section | 29/09/2022 | 2022-1766 | 29/09/2022 | 29/09/2022 | Articles Abstract Database |