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NASA Technical Reports Server (NTRS) 20060014041: Applications of Clocks to Space Navigation & "Planetary GPS" PDF

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y y or og at ol r n o h b ec r a T e n L e of nd io ut u uls stit ” y, rop nia In S og P or P ol et alif G n J C h c y e T r a f o t e e t n u t a ti s l n P I “ a i n & r o if n aln o Co i t i ,a t yr a rt os g atni vi ormi bd a aA N L n e onc e ioa c ctsip a eulS Spd p s on S nPra o o tiet cs s t yplicahe Jnauti ck or Apat tero o atndut A Cl n ors ad onal 4 bmeo tions of 0, 200 M. Lichte sion Laking Systeh was carriith the Nati ca 2 n pulTracearcct w ppli pril phe Proger, s resontra A A e t nahi c t eaTa S JM * y y 2 tor olog en - ora echn s Licht Lab e of T die S”ion stitut bo s n Ppul nia I y Go or ar Pr alif t aryJet C ane t e pl n n r o a e i Pl h at t g “ h o & rt at avi a n E s n / o m g t ti n a e n a o n t ki vig ati tio sys rac Na nt ga n d t e o ce es avi ati an a r n g s p P d vi m S f n a e o a n t to e g S s/ ys n n s s n P i o ck utli ack G ati ary o O r or c t l t i e C r f g n n o s n u a of f ck ki m pl s s” o ac m e cation S “work ce of cl ace Tr s for co GPS-lik li P n p t p a S p Ap w G port ep nce arse o m e o p H D C S I • • • • • y y 3 tor olog en - ora echn Licht b T La e of n ut S”io stit s n Pul a I p ni Go or Pr alif y C arJet t e n a l P “ & e d ion telliteniquem co gats S saa undo viork GPits ora a m W d N hsu e S acanse Erp cP t a G p Sw o o Applications of Clocks tH GPS determines user position via“triangulation” to three GPS satellites The user’s GPS receiver compareseach satellite’s unique pseudorandomcode to models stored in the receiver tomeasure the time delay, and hencedistance, to each GPS satellite –Requires that all GPS satellites be“synchronized” to “same” time –User does not need a good clock: afourth GPS measurement determinesthe user time offset from “GPS time” Each GPS satellite continuouslybroadcasts its ephemeris and offsetfrom “GPS time,” which is definedprecisely relative to highly stableground clocks. With these data, a GPSuser receiver can in real-time uniquelydetermine its location (and time offsetfrom “GPS time”) by tracking four GPSsatellites • • • y y 4 tor olog en - ora echn Licht b T La e of CS n ut M S”sio nstit S Pul a I P Gop orni G Pr alif y C arJet t e n t a a a m t ce Navigation & “Pl Works (cont.) (OCS). The USAF trol Station (MCS) ngs, plus monitor ajalein, Diego Garci ons passively track w. The MCS ellite’s ephemeris dically uploads the in its navigation e updated every eriod, the broadcas ately because … haved orbits ugh the very stable ground Applications of Clocks to Spa How GPS perational Control Segment CS consists of one Master Con hriever AFB in Colorado Spri ations at the MCS, Hawaii, Kw d Ascension Island. The stati nging data from all GPS in vie timates and predicts each sat d clock parameters and perio each GPS for re-transmission essage. PS ephemeris/clock uploads ar veral hours. During that time p hemeris degrades only moder GPS are in relatively high-altitude, well-be GPS all carry precise (atomic) clocks Knowledge of GPS time is maintained throclocks at the ground tracking sites c n s n e p O O S st a a e a o m G s e – – – r t • • y y 5 tor olog en - ora echn Licht b T La e of CS n ut M S”sio nstit S Pul a I P Gop orni G Pr alif y C arJet t e n y d la es sl n & “P ers g sit nuou mple st a nts nt d n gn kin nti si bu me me an atio nt.) esi trac d co vely ro eg eg le ) ce Navig Works (co e GPS d nal ground curately an nd clocks arries relati ood clock invest in control s e user s vely simp in 1980s Applications of Clocks to Spa How GPS e Design Trade for GPS. Th orporated … Accurate (atomic) clocks at operatio and onboard the GPS satellites A 24/7 global tracking network to ac determine and update GPS orbits a In contrast: the GPS user typically c equipment and does not require a g e U.S. government elected to able GPS space and ground/ rastructure), thus enabling th llions of users) to carry relati eap user equipment ughly $12B to develop GPS ( h c h li nf mi h o T n – – – T e i c R i r ( ( • • • y y 6 tor olog en - ora echn Licht b T La e of n ut S”io stit s n Pul a I p ni Go or Pr alif y C arJet t . ne cks bal ks. Pla c.) ial al clo glo cloc on & “ day oats et different em differenti dence on equires dence on ati o b al st al en ng R en ce Navig mance T eld, autos, t modeling. vices ocal/region t modeling. DGPS) sy quires glob iminates dep c positioni g accuracy. minates dep Applications of Clocks to Spa GPS Perfor one commercial receiver (handh eters real-time positioning. erformance is limited by GPS clock & orbi rcial receiver with differential ser ters real-time positioning. Requires lce subscription. erformance is limited by GPS clock & orbi cision global differential GPS (G m real-time positioning accuracy. Rece from commercial partner. etwork processing improves orbits and el l-time (minutes to days) geodeti r than 1-cm non-real-time positioninork data + special software. etwork processing improves orbits and eli dal 0 m P me meervi P pre 0 cervi N rea etteetw N n 1 • m 2 s • L 1s • n- Bn • a o P o t – – – – S C N J • • • • y y 7 tary GPS”Jet Propulsion Laborators California Institute of Technolog 1-cm accuracy GRACE Mar 2002 nt >12 years of on-orbit performance Lichten - e e r n e m a v p l ei y 1 1 o “P c ac N- 00 el M e ur O 2 v 8 T ace Navigation & L Blackjack GPS R ality clocks (USOs). ccuracy1-cm accreal-time demoC-C JAS 2000 Dec Missions In De 2005 200 MIC OS Sp JP h-qu m ameter SA Nov ept OS s of Clocks to avigation with receivers carried hig accuracy4-cSub-HAMP l 2000 002 S Sat C uracy n N PS m C Ju 2 E cc catio ecraft RACE G 4-c Dec IC 5-cm a Appli Spac ese, only the G accuracy TM 2000 2 t h m R b 0 a all t 5-c S Fe 20 dS Of 4 ec e D F y y 8 tor olog en - ora echn Licht b T La e of n ut S”io stit s n Pul a I p ni Go or Pr alif aryJet C nas t e n n h e t a t n l r a P a “ E m & - 4 g m n 3 n o o d i tik r n ac f a g a g m I i B avTr n 0- L i N k 7 V e e c s , ay c a e e c l aa r s g e Spp e t k u /s an m d o S c or h m r c tp a w rt m s ay 2 s e p et Ea rs s 3 er w 1. ClockDe ep s ce N bility om o Ma n ssue s 0.0 met one- ec = ons of of de als eep Spa and visi l time fr minutes t c to Moo frame i a type Doppler, ange, 2 rential 0.06 ns vigation ati es gn A D ry ve 5 se ce at y y r ffe d = na pplic eng ak si NAS omet ht tra 5 to 2 ~ 1.3 eren al d o-wa o-wa ta-Di 2 nra ical A l e e g ef c w w el pt l a W • G Li • • R pi T T D • O h y C – – – – T – – – – • • y y 9 tor olog en - ora echn Licht b T La e of n ut S”io stit s n Pul a I p ni Go or Pr alif y C arJet t e n s a e l i P d o “ B & y n r a o t i e t a n g a i Pl v a r N e d h & e t e ? c O vn s ut a t oo n r b y Sp g a pratigs o Ma in, full Applications of Clocks to “In Situ” Trackin e MER mission dramaticallye high value of having navigecom “infrastructure” durinallenging surface operationher planetary bodies hat is the best approach for r the Moon? Light travel time to Mars is tens of monly about 1 sec to the Moon •Importance of autonomy Some Earth-orbiting GPS can be useracked at Moon h lh o t Thecot WF • • tt • • s & “Planetary GPS”Jet Propulsion Laboratory California Institute of Technology s Infrastructure Other Mars Orbiter or low Mars orbit vehicle can bewith 1-way Doppler mance depends on user’s clock ocks, 1 orbiter only: 3 km in 24 hrs ocks, 1 orbiter only: 300 m in 24 hr cking two orbiters simultaneously,dence on user’s clock is reducedminated nd angle-sensing may improvemance or robustness e challenging if target vehicle isuvering Lichten - 10 ation biters a urface acked Perfor -810 cl -910 cl By tradepenor eli IMU aperfor Can bmane g Or y Sr • • • • • • a t i w v m • - a o 1 N C / v e a c N a S 2 p R r S o A 1 M o h t t i s W k s c r o a M l C t a f o e l s c n hi y o e a i V w U at a 1- M d c g I r li n e a p i v o k p c ti b A a c n r A o T r e t i b r O

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