dc.contributor.author |
Saratayon, Peerayudh |
|
dc.contributor.author |
Petchartee, Somrak |
|
dc.date.accessioned |
2563-08-25T08:32:01Z |
|
dc.date.available |
2563-08-25T08:32:01Z |
|
dc.date.issued |
2558 |
|
dc.identifier.uri |
http://hdl.handle.net/123456789/1947 |
|
dc.description |
บทความวิจัย |
en_US |
dc.description.abstract |
This article demonstrates the design methodology
based on Software Defined Radio (SDR), the result of which
proves the flexibility of this method. Reconstructable IRIG
datagram are presented without the need to reconfigure the
receiver. Some of the functions of commutator/decommutator
desired by the platform include missile telemetry, temperature
and pressure measurement, GPS location transmission and a
continuous sensor-data feed of sensor and missile status. |
en_US |
dc.description.sponsorship |
Defence Technology Institute |
en_US |
dc.language.iso |
en |
en_US |
dc.publisher |
Defence Technology Institute |
en_US |
dc.relation.ispartofseries |
58059; |
|
dc.subject |
IRIG106 |
en_US |
dc.subject |
SDR |
en_US |
dc.subject |
Telemetry |
en_US |
dc.subject |
Missile |
en_US |
dc.subject |
Commutator |
en_US |
dc.subject |
Decommutator |
en_US |
dc.title |
IRIG S-Band Missile Telemetry |
en_US |
dc.type |
Article |
en_US |