The Mars Exploration Rover Surface Mobility Flight Software: Driving Ambition

Total Page:16

File Type:pdf, Size:1020Kb

The Mars Exploration Rover Surface Mobility Flight Software: Driving Ambition Published in 2006 IEEE Aerospace Conference Proceedings, March 2006, Big Sky, Montana, USA The Mars Exploration Rover Surface Mobility Flight Software: Driving Ambition Jeffrey J. Biesiadecki and Mark W. Maimone Jet Propulsion Laboratory Pasadena, CA USA [email protected] [email protected] Abstract— AUTONOMOUS GOAL SELECTION 10 6 DEPLOYMENT RESULTS 10 NASA’s Mars Exploration Rovers’ (MER) onboard Mo- SOFTWARE VERSIONS 11 bility Flight Software was designed to provide robust and flexible operation. The MER vehicles can be commanded 7 CONCLUSION 13 directly, or given autonomous control over multiple aspects 8 ACKNOWLEDGEMENTS 13 of mobility: which motions to drive, measurement of actual motion, terrain interpretation, even the selection of targets of 1. INTRODUCTION interest (although this mode remains largely underused). Vehicle motion can be commanded using multiple layers of control: Motor Control, Direct Drive operations (Arc, Turn in Place), and Goal-based Driving (Goto Waypoint). Multiple layers of safety checks ensure vehicle performance: Com- mand limits (command timeout, time of day limit, software enable, activity constraints), Reactive checks (e.g., motor cur- rent limit, vehicle tilt limit), and Predictive checks (e.g., Step, Tilt, Roughness hazards). From January 2004 through October 2005, Spirit accu- mulated over 5000 meters and Opportunity 6000 meters of odometry, often covering more than 100 meters in a single day. In this paper we describe the software that has driven these rovers more than a combined 11,000 meters over the Martian surface, including its design and implementation, and summarize current mobility performance results from Mars. Figure 1. Mars Exploration Rover. Keywords— ¢¡¤£¦¥¨§ © © ¥ ¢§§ © §¥ "! # $ ©%&(')§*¥ §*© +©-,© .0/""(1¥23 © 4.©,5© 2674689"!: 0©4;¥%<2./"=.§ © > 0©4;¥ DFEHG3EI 26A*J%K2./"/01H/046@3@L('M©N,5© 6"/0§*© +©;! ©/0©! 0J*O© 4 90 26/?©9@.©,5A*§ 1 ¥3!© ,5© 0©4 #6H 2.§ %<AP©%; ¢§*M04RQ:4926§*1STTU6VW*#.LG9=.0§ ")46@YXP=.Z =+©§ 2.4."(1[ ¢§*¡¨\3=./0©§*"© 4[£N©§*R]< ¢¡M£F^>_`)#."§5=.§*"Z ,a§*1b! © /c0$ ©Id646@e:@346A¢©%¦=6Jf')*§RYgH26 h TABLE OF CONTENTS § §P46@i j§ @34.-k/492.,l¥+('m©$!©/0©!/"/[email protected] 046> n*o©4p©=.=+© " qJ@3o©%$ #.q=./46A_rEc/" #.© 2.!#s #6 1 INTRODUCTION 1 #6",54 a©%P*#.0§R 26*(%K26/c/046@304.! aJ*[email protected]© 23R 2 MER FLIGHT SOFTWARE ARCHITECTURE 2 i #64.©/0©! 0/*©2.§5@3Y%K©§A ¥¨n5t*#.0§a .0/0n(1u*©i*§*Z 3 MOBILITY MANAGER SOFTWARE 3 §* )'N#.0/"N© 4v*#.F 2.§ %<A)©%O ¢§*7*#6M#6¨46 6/"@v +©*# §*©§¤ ©$ 26@R04R*#.0§N=.§*",a§ 1$! © /0_ 4 LOW-LEVEL DRIVING 4 5 AUTONOMOUS DRIVING 5 `)#.m ¢¡¤£w§*©§*?§ (1:=60/0/"1xA© ,,a46@3@¦©46= §7 i§ Z PRIMARY AUTONOMOUS CAPABILITIES 5 4¢@681_cEy z:2.46AL©%¤A© ,,[email protected] 4:P04l #6t,5©§*4.04.! = A"d6¦ #.f@681+{ ¦ > 09n*"V'N#6t",a!t46@w@.*Y*© ERRAIN SSESSMENT VERVIEW T A O 7 A© /"/0A¥O#.©'| ©R= ©:J" 0©4¢ #.v§ © © t§*,a¥O4 @j'N#.§*L*© ROBUST STEREO IMAGE PROCESSING 8 @3§*" _-`)#.4R¤*#.F46@a©%O#[email protected] ¥*#.F§*©§*¨ 4 @a 6} TERRAIN ASSESSMENT 8 #6$",a!v46@u@.*j#92.,a4w©=+§ © §*x'N0/0/¤26 a ©i=./04 #6t4.\:[email protected]{ FA 09n*"_H`)#.t4.\[email protected]{ c,5© .0/0n(1jA© ,Z ,a46@6c§*LJ/"> @f @Y©4Y'N#6cN}94.©'N4f~f46@Y'N#6 B 0-7803-9546-8/06/$20.00 C c 2006 IEEE 1 4/' 4.§J*0/. j J2.§*,54 10c46n*#6¨#6 Z \37 /0§*©,Z )2.4.}94.©'N4R~f +©23) #6x §*§04Y#. @?_ A*§¨46@ Z \374.!26/0§7§*m 4 J© §*_2' 45 ('M45@3§*"904.! =.§*",5" 0¥+ #6v§*©§F4¢,a}t26J©%¤,5§Z 6 J@)%PnZ `)#.§ © §F§ 5@3§*" 4¢26 04.!f*#.§*5=.§*",a§*1l,5©[email protected]/0©')Z 26/XH@3©,5 §*1u] 23*©4.© ,5©26F §}904.!$©%M",a! ¦%K 26§ /0/¨A©,5,a4 @.P #6L =+A"%K1¢\3 >*/"1l#.©' ,v26# ©R 2.§*4 4 @jJ2. Jz 264:P§*©§N,© 0©4j(*",a*"© 4 ^)*©fA© § §*Ac #6 #x'N#./ 4 @P=+© " 0©4¦J § 04.!c > 2 © §*¥@."§*A @L@.§ 0:Z §*§*©§04$ #6P04." /?'N#./O©3@3©,5A*§ 1:Z 6 @5(*",a P #6 04.!i=.§*0," 0L%K© §v@3§*"904.!i/"© 4.!iA0§A2./§t§*f]<©%c'N#.# ©32.§x'N#.4i #.5'N#./x/"©:Jt §>*"© 4i© 4i/§*!t§*©3}3P46@ J §0!#:/"04.H@3§ 09"46!¦46@*2.§ 4.Z 043Z =./0 AF§ c =+A/+ J*^A¥ J =[J/0©=+_3%P0 26/)XH@3© , §*1 ©%&(')§*¥W46©t© § 0!046/0/01 4 @e23*©4.© ,© 26a=6 # /0A 0©4W_¢¡;©')Z /0 /F©,5,a46@6 =6§J5©%c*#.l 6 /004.R@3J0!4b .23a046A© § =+©§*@[ £ A\9 § 4 ./0¤£J4.© 43Z (46@.§*@¦¥M > 09n*"; 26#L?2 J04.!) #6'N#./0 A§*@.n ¥.¥#6 -!46§ @L©§-S T TFA© ,t .04.@v 26*(%K26/:=+©Z ©b@3"!I#.©/0f"4 ¢§J*04 J© "/ ¥N 2¨§ § ©3}3¥N46@q= §J%K© § , n*"© 4R2.=O@. c©4l © #l§*©§4 _ ,5#64.J, #./n*#I@3! 4.© J (_ ©P0§ > @[@3§*" v/"Z /0©' #92.,a4q© = §* ©§ ©[ =+A"%K1 A\.A /01I'N#.# @3§*"904.! =.§*",5" 0m #.¦§*©§M'N0/0/W= §J%K© § ,l_EF23 © 4.©,5©2 N=6*#jJZ 2. MER FLIGHT SOFTWARE ARCHITECTURE /0>*"© 4[,5©3@3Y/"/0©'cL*#.Y§ © §¦*©¢}Rn5A2.§*§ 4:v(* `)#. ©§/0/f§*#." >*2.§ ©%j #6| ¢¡M£ 60!#: ©%&(')§* 04 *©fA© 2.4:F'N#.4¢ /0A 04.!$'N#.#i@3§*0:04.!a=.§*0," 0N*© ')P 6 @i©4¢*#6L26 @¢%K©§H #6 ¢§*xk¨ #3d64 @3§H/046@3§ h A\3A23*¦ ©R,5©§*¦ §OA 0/01l§ #¢ § 4l!©:/;/0©3Z ]< ik65¨^>¥O46@Y*#.v©,5,a46@j46@Y /",5A §*1Y"43%K§J §*26A 2.§* 0©4j 2.=.=./00@Y 91$#92.,a4Y©=+§ © §*_ 04j=6§ A2./§F#6@j "! 4."d 4 F@. "! 4l46@l0,=6/",4:**"© 4 04.#.§*"*4 A_ `)#.q,5© .0/0n(1pJ13J , #6w n\ S A4:*",5A*§[email protected], § 'N#./¥O©%'N#60#j*#.v%K©2.§xA© § 4.§F'N#./F,a81l +J §*@ $m©*# ¢k75q/046@3§x4 @i ¢¡M£ §*©§N26 v #.5A© ,,5§*0/ ~s ,5#64./$©43d !2.§*"© 4s@3§ 0@y%K§*©, #. i§ ©=+§*"46!u 13(*,8%F\¨ © § }3%K§*©,8e046@q£N0§_ `)#.50 k¨*#3d646@.§Y§ © §YG3©(©26§ 4.§ _ `)#. §*©§f +©3@31 #6 ¦=6§ Z ,=. 0F,v2./" "Z }:04.!aXxGa26 @$%K©§m,5491§*/nZ 0,5 TiA4:*",5A*§v!§*©2.46@w/"§46¥-46@u/§*!$ ©/§v=646/ 19J ,a;4 @LJ=6 AA§%&_ ¢¡¤£w,5=./"©13O*#.M*,5¤£FE9©4 : ©4[ #.f ©=I©%N #6f§*©§t§ z 26"§*f@6@3n*"© 46/mA/0§*46A5*© 60!#:7©,5=.23*§7W2 J@L 91F*#.m ik65R/046@3§m]</n*#.©2.! #L #6 */"/M§ ©3}3a] T¢A4: 0, §*x%K§*©, !§*©2646@ ©i ©/§L=64./&^>_ ¢¡M£o/"©3}P§ 2.4 W STN +.-# ¥%K© 2.§?*",5?%<J §W #64¦ ¢k65¨^>¥ e#./- 6 /004.¦F§*©2.! #./01v, §H [email protected] ©Z 0@3v46@ _ S 4 @l#6c&%H ¢¡e04: § %<x ©f §/? +© §*@.m*#6HA©4:*§ © / ,5A*§-%K§ © 4:JZ ©Z 6 }+_7`)#.F ¢¡M£q§ © §-4*2.§ 4a04$=./ ,5©*©§¥9§@30© ¥:,5§¥946@R "46AH"4 (*§ 2.,54 _G9© ,5 +©2.oe=+©04: +A('m4 #.I('M© ,5@.@3/0b'N#6/¥v@3§*" ©%P #.;%H ¢¡p ©:§@.#68l §*0/m04: §J%< A*©u© #6§a@3AZ J §0!#:W%K©§*')§@x©§; }9'm§*@W¥46@L#68 ¤- (-c© 4.¤,5AZ 90¥"4:*§ %<A@x ©P #6¤60!#:¨A© ,=623 § 91L')81P©%<5-kMgxEF §H 2.§*4¢§@3026F%K©§L@3§*"904.!R/"© 4.!fA0§A2./§x§_xG9 §0!#: # m©4.46>*@5 +©*#a #.9%P ¢¡I .26¤46@5*#.F §*0/6 .26* _ /0"4.x@3§*"904.!v =+@f0) Am © _ ¦4: 0,5A*§ JA©4 @?¥ 46@ `)#.§ N§*4S,H j 91: -©%=©P£cEP 46@5S P j 91: -©% # #6a§ © §c*2.§ 4o04o=6/0 Aa¦§*©2.! #./01iS3_!5@.!§* JA© 46@?_ ,5,5©§*1¥346@ j 91: m©%7¡M¡¤kM£NXH [_:`)#.L j© .0/""(1a* J} `)#.R§ © §L§*f(*0/0/"1wJ* 6/"f¢ 0/n©%cU" ¢@3! § ¥ ]<@.*A§*" +@f /"©'F^MM! " 43, T>:x 91: ¤©%7J* }+¥94 @f4.© ,Z #.©'m §5@3§ 09"46!o© 4q,© § Y*#64 Tu@3!§*lJ/0©=+a54.© 046/0/"1? j! :1:*x©%c@3@3*@o#.=[ =6l]<©%N'N#.# §*A© ,5,46@3@[email protected]*©¦ #6F=+© *J0 .0/""(1v©%?2.46A© 4: §*©/0/"@ /00@9Z v,©:(/Y ¢ :1:*¦# L +4w26J@?¥-L©%FXHA © §vST T ^A_ 04.!6_f£c©9}3H/0/"§L #64wl'N#./¤§*aA©4 J@3§*@ ,5© .0/0n(1 `)#.F6"! #:m ©%&(')§*NnJ/n%;§*z:2.0§*A@v j 91 *¥ ©%W'N#.#+_ U #6 #§@._ j 91: )0N2 J@f 91$*#.tG92.§ %<LDF89"!:*"© 4f,5©3@32./0_ $m©*#u@."§*A @w46@o=6*#[J/">*"© 4o,5©3@3¦©%c@3§*0:04.!j4 ¡W0} ¢k65m¥+ #6 ¢¡M£y ©%&(')§*¦P@3090@.@ "4: ©R#.0!#3Z /"/ ,a} P26 x©%7©43Z ©:§@fG:*§*©&%FJ0©4Y=.§*©3A* "4.!46@Y` § Z © B(>_¨¡M#$/"> §*©[email protected]!4.§/0/"15§*=.§* 4:*@ §04bEc4 /019 ©%&(')§*a*©[email protected] § ,504.Y'N#.A*#.§5*#.R§*©§ 91v4© ¨(A¥ 'N#."/0F @.@3" 0©46/.J©%&('m§ Z © 4./"1L© ¨(A*¨=6§ ©Z 'm©2./@L4 A©264 *§-491H!© ,5A §*¨#6#§@.; ;"¨@3§ 0;/"© 4.! [email protected]%K§J §*26>*2.§*l §*90v ©o*#.l§ (a©%P #.j,5©3@32./0 "*x#.© 4i=6*#W_(' 4 @."§*A @ @3§*"904.!6¥O*#.v§*©§P4i=6§ Z ]&%K© §A\.,=6/" ¥§*A© §*@."4.!P /",5A §*1t,5 2.§ ,54:*-© §(*©§ Z ,5=3*" /01)¥A*©¥5a = A"d L,5© .0/0n(1YA©,5,a4 @Y%K§ © , #6 04.!a( L04l4.©49 ©/ 0/0P,5,5© § 1.^>_ !§*©2646@j"%¤n¦=.= §N*©:©Y§*0 }91_*' 4 EF23 © 4.©,5©2 PDP8:0! Z 0©4$] Ec23*©468.^;46@x© #.§;=6 #t /0A 0©4L,5©3@3¥ #.§*©§ ¡¤ #[J©%&('m§ f© ¨(>v# ¦"*©'N4u*#.§ @w©%FA© 4 *§ © / ¥-© § 4R /0Am"*)©'N4f@.§ 09"4.!=.§*",5" 0¤*©J §)§*©2.4 @$© .Z * J}O_¨¡¤ #$© B(>N#6 mn)©'N4R AN©% J* x§*0 ./0¥:46@ J*/"4 @v,a}N=.§*©! § ©')§@vn!©:/ _ `)#.¤ ©%&(')§* @3©9t4.©5J# §*a,,5©§*1 'N" #[© #.§t© ¨(A*_;' 46(* @u©% =.§*©90@3a*#.i2.460z:2.o= .0/""(1q©%¦46 ./004.!w #6 #.A/0 #6§*"46!j,,5©§*1¥7© ¨(>*vA© ,,v2.4.
Recommended publications
  • Planetary Report Report
    The PLANETARYPLANETARY REPORT REPORT Volume XXIX Number 1 January/February 2009 Beyond The Moon From The Editor he Internet has transformed the way science is On the Cover: Tdone—even in the realm of “rocket science”— The United States has the opportunity to unify and inspire the and now anyone can make a real contribution, as world’s spacefaring nations to create a future brightened by long as you have the will to give your best. new goals, such as the human exploration of Mars and near- In this issue, you’ll read about a group of amateurs Earth asteroids. Inset: American astronaut Peggy A. Whitson who are helping professional researchers explore and Russian cosmonaut Yuri I. Malenchenko try out training Mars online, encouraged by Mars Exploration versions of Russian Orlan spacesuits. Background: The High Rovers Project Scientist Steve Squyres and Plane- Resolution Camera on Mars Express took this snapshot of tary Society President Jim Bell (who is also head Candor Chasma, a valley in the northern part of Valles of the rovers’ Pancam team.) Marineris, on July 6, 2006. Images: Gagarin Cosmonaut Training This new Internet-enabled fun is not the first, Center. Background: ESA nor will it be the only, way people can participate in planetary exploration. The Planetary Society has been encouraging our members to contribute Background: their minds and energy to science since 1984, A dust storm blurs the sky above a volcanic caldera in this image when the Pallas Project helped to determine the taken by the Mars Color Imager on Mars Reconnaissance Orbiter shape of a main-belt asteroid.
    [Show full text]
  • Mars, the Nearest Habitable World – a Comprehensive Program for Future Mars Exploration
    Mars, the Nearest Habitable World – A Comprehensive Program for Future Mars Exploration Report by the NASA Mars Architecture Strategy Working Group (MASWG) November 2020 Front Cover: Artist Concepts Top (Artist concepts, left to right): Early Mars1; Molecules in Space2; Astronaut and Rover on Mars1; Exo-Planet System1. Bottom: Pillinger Point, Endeavour Crater, as imaged by the Opportunity rover1. Credits: 1NASA; 2Discovery Magazine Citation: Mars Architecture Strategy Working Group (MASWG), Jakosky, B. M., et al. (2020). Mars, the Nearest Habitable World—A Comprehensive Program for Future Mars Exploration. MASWG Members • Bruce Jakosky, University of Colorado (chair) • Richard Zurek, Mars Program Office, JPL (co-chair) • Shane Byrne, University of Arizona • Wendy Calvin, University of Nevada, Reno • Shannon Curry, University of California, Berkeley • Bethany Ehlmann, California Institute of Technology • Jennifer Eigenbrode, NASA/Goddard Space Flight Center • Tori Hoehler, NASA/Ames Research Center • Briony Horgan, Purdue University • Scott Hubbard, Stanford University • Tom McCollom, University of Colorado • John Mustard, Brown University • Nathaniel Putzig, Planetary Science Institute • Michelle Rucker, NASA/JSC • Michael Wolff, Space Science Institute • Robin Wordsworth, Harvard University Ex Officio • Michael Meyer, NASA Headquarters ii Mars, the Nearest Habitable World October 2020 MASWG Table of Contents Mars, the Nearest Habitable World – A Comprehensive Program for Future Mars Exploration Table of Contents EXECUTIVE SUMMARY ..........................................................................................................................
    [Show full text]
  • THE MARS 2020 ROVER ENGINEERING CAMERAS. J. N. Maki1, C
    51st Lunar and Planetary Science Conference (2020) 2663.pdf THE MARS 2020 ROVER ENGINEERING CAMERAS. J. N. Maki1, C. M. McKinney1, R. G. Willson1, R. G. Sellar1, D. S. Copley-Woods1, M. Valvo1, T. Goodsall1, J. McGuire1, K. Singh1, T. E. Litwin1, R. G. Deen1, A. Cul- ver1, N. Ruoff1, D. Petrizzo1, 1Jet Propulsion Laboratory, California Institute of Technology (4800 Oak Grove Drive, Pasadena, CA 91109, [email protected]). Introduction: The Mars 2020 Rover is equipped pairs (the Cachecam, a monoscopic camera, is an ex- with a neXt-generation engineering camera imaging ception). The Mars 2020 engineering cameras are system that represents a significant upgrade over the packaged into a single, compact camera head (see fig- previous Navcam/Hazcam cameras flown on MER and ure 1). MSL [1,2]. The Mars 2020 engineering cameras ac- quire color images with wider fields of view and high- er angular/spatial resolution than previous rover engi- neering cameras. Additionally, the Mars 2020 rover will carry a new camera type dedicated to sample op- erations: the Cachecam. History: The previous generation of Navcams and Hazcams, known collectively as the engineering cam- eras, were designed in the early 2000s as part of the Mars Exploration Rover (MER) program. A total of Figure 1. Flight Navcam (left), Flight Hazcam (middle), 36 individual MER-style cameras have flown to Mars and flight Cachecam (right). The Cachecam optical assem- on five separate NASA spacecraft (3 rovers and 2 bly includes an illuminator and fold mirror. landers) [1-6]. The MER/MSL cameras were built in two separate production runs: the original MER run Each of the Mars 2020 engineering cameras utilize a (2003) and a second, build-to-print run for the Mars 20 megapixel OnSemi (CMOSIS) CMOS sensor Science Laboratory (MSL) mission in 2008.
    [Show full text]
  • Long-Range Rovers for Mars Exploration and Sample Return
    2001-01-2138 Long-Range Rovers for Mars Exploration and Sample Return Joe C. Parrish NASA Headquarters ABSTRACT This paper discusses long-range rovers to be flown as part of NASA’s newly reformulated Mars Exploration Program (MEP). These rovers are currently scheduled for launch first in 2007 as part of a joint science and technology mission, and then again in 2011 as part of a planned Mars Sample Return (MSR) mission. These rovers are characterized by substantially longer range capability than their predecessors in the 1997 Mars Pathfinder and 2003 Mars Exploration Rover (MER) missions. Topics addressed in this paper include the rover mission objectives, key design features, and Figure 1: Rover Size Comparison (Mars Pathfinder, Mars Exploration technologies. Rover, ’07 Smart Lander/Mobile Laboratory) INTRODUCTION NASA is leading a multinational program to explore above, below, and on the surface of Mars. A new The first of these rovers, the Smart Lander/Mobile architecture for the Mars Exploration Program has Laboratory (SLML) is scheduled for launch in 2007. The recently been announced [1], and it incorporates a current program baseline is to use this mission as a joint number of missions through the rest of this decade and science and technology mission that will contribute into the next. Among those missions are ambitious plans directly toward sample return missions planned for the to land rovers on the surface of Mars, with several turn of the decade. These sample return missions may purposes: (1) perform scientific explorations of the involve a rover of almost identical architecture to the surface; (2) demonstrate critical technologies for 2007 rover, except for the need to cache samples and collection, caching, and return of samples to Earth; (3) support their delivery into orbit for subsequent return to evaluate the suitability of the planet for potential manned Earth.
    [Show full text]
  • GRAIL Twins Toast New Year from Lunar Orbit
    Jet JANUARY Propulsion 2012 Laboratory VOLUME 42 NUMBER 1 GRAIL twins toast new year from Three-month ‘formation flying’ mission will By Mark Whalen lunar orbit study the moon from crust to core Above: The GRAIL team celebrates with cake and apple cider. Right: Celebrating said. “So it does take a lot of planning, a lot of test- the other spacecraft will accelerate towards that moun- GRAIL-A’s Jan. 1 lunar orbit insertion are, from left, Maria Zuber, GRAIL principal ing and then a lot of small maneuvers in order to get tain to measure it. The change in the distance between investigator, Massachusetts Institute of Technology; Charles Elachi, JPL director; ready to set up to get into this big maneuver when we the two is noted, from which gravity can be inferred. Jim Green, NASA director of planetary science. go into orbit around the moon.” One of the things that make GRAIL unique, Hoffman JPL’s Gravity Recovery and Interior Laboratory (GRAIL) A series of engine burns is planned to circularize said, is that it’s the first formation flying of two spacecraft mission celebrated the new year with successful main the twins’ orbit, reducing their orbital period to a little around any body other than Earth. “That’s one of the engine burns to place its twin spacecraft in a perfectly more than two hours before beginning the mission’s biggest challenges we have, and it’s what makes this an synchronized orbit around the moon. 82-day science phase. “If these all go as planned, we exciting mission,” he said.
    [Show full text]
  • Educator's Guide
    EDUCATOR’S GUIDE ABOUT THE FILM Dear Educator, “ROVING MARS”is an exciting adventure that This movie details the development of Spirit and follows the journey of NASA’s Mars Exploration Opportunity from their assembly through their Rovers through the eyes of scientists and engineers fantastic discoveries, discoveries that have set the at the Jet Propulsion Laboratory and Steve Squyres, pace for a whole new era of Mars exploration: from the lead science investigator from Cornell University. the search for habitats to the search for past or present Their collective dream of Mars exploration came life… and maybe even to human exploration one day. true when two rovers landed on Mars and began Having lasted many times longer than their original their scientific quest to understand whether Mars plan of 90 Martian days (sols), Spirit and Opportunity ever could have been a habitat for life. have confirmed that water persisted on Mars, and Since the 1960s, when humans began sending the that a Martian habitat for life is a possibility. While first tentative interplanetary probes out into the solar they continue their studies, what lies ahead are system, two-thirds of all missions to Mars have NASA missions that not only “follow the water” on failed. The technical challenges are tremendous: Mars, but also “follow the carbon,” a building block building robots that can withstand the tremendous of life. In the next decade, precision landers and shaking of launch; six months in the deep cold of rovers may even search for evidence of life itself, space; a hurtling descent through the atmosphere either signs of past microbial life in the rock record (going from 10,000 miles per hour to 0 in only six or signs of past or present life where reserves of minutes!); bouncing as high as a three-story building water ice lie beneath the Martian surface today.
    [Show full text]
  • NUCLEAR SAFETY LAUNCH APPROVAL: MULTI-MISSION LESSONS LEARNED Yale Chang the Johns Hopkins University Applied Physics Laboratory
    ANS NETS 2018 – Nuclear and Emerging Technologies for Space Las Vegas, NV, February 26 – March 1, 2018, on CD-ROM, American Nuclear Society, LaGrange Park, IL (2018) NUCLEAR SAFETY LAUNCH APPROVAL: MULTI-MISSION LESSONS LEARNED Yale Chang The Johns Hopkins University Applied Physics Laboratory, 11100 Johns Hopkins Rd, Laurel, MD 20723 240-228-5724; [email protected] Launching a NASA radioisotope power system (RPS) trajectory to Saturn used a Venus-Venus-Earth-Jupiter mission requires compliance with two Federal mandates: Gravity Assist (VVEJGA) maneuver, where the Earth the National Environmental Policy Act of 1969 (NEPA) Gravity Assist (EGA) flyby was the primary nuclear safety and launch approval (LA), as directed by Presidential focus of NASA, the U.S. Department of Energy (DOE), the Directive/National Security Council Memorandum 25. Cassini Interagency Nuclear Safety Review Panel Nuclear safety launch approval lessons learned from (INSRP), and the public alike. A solid propellant fire test multiple NASA RPS missions, one Russian RPS mission, campaign addressed the MPF finding and led in part to two non-RPS launch accidents, and several solid the retrofit solid propellant breakup systems (BUSs) propellant fire test campaigns since 1996 are shown to designed and carried by MER-A and MER-B spacecraft have contributed to an ever-growing body of knowledge. and the deployment of plutonium detectors in the launch The launch accidents can be viewed as “unplanned area for PNH. The PNH mission decreased the calendar experiments” that provided real-world data. Lessons length of the NEPA/LA processes to less than 4 years by learned from the nuclear safety launch approval effort of incorporating lessons learned from previous missions and each mission or launch accident, and how they were tests in its spacecraft and mission designs and their applied to improve the NEPA/LA processes and nuclear NEPA/LA processes.
    [Show full text]
  • Operation and Performance of the Mars Exploration Rover Imaging System on the Martian Surface
    Operation and Performance of the Mars Exploration Rover Imaging System on the Martian Surface Justin N. Maki Jet Propulsion Laboratory California Institute of Technology Pasadena, CA USA [email protected] Todd Litwin, Mark Schwochert Jet Propulsion Laboratory California Institute of Technology Pasadena, CA USA Ken Herkenhoff United States Geological Survey Flagstaff, AZ USA Abstract - The Imaging System on the Mars Exploration Rovers has successfully operated on the surface of Mars for over one Earth year. The acquisition of hundreds of panoramas and tens of thousands of stereo pairs has enabled the rovers to explore Mars at a level of detail unprecedented in the history of space exploration. In addition to providing scientific value, the images also play a key role in the daily tactical operation of the rovers. The mobile nature of the MER surface mission requires extensive use of the imaging system for traverse planning, rover localization, remote sensing instrument targeting, and robotic arm placement. Each of these activity types requires a different set of data compression rates, surface Figure 1. The Mars Exploration Spirit Rover, as viewed by coverage, and image acquisition strategies. An overview the Navcam shortly after lander egress early in the mission. of the surface imaging activities is provided, along with a presents an overview of the operation and performance of summary of the image data acquired to date. the MER Imaging System. Keywords: Imaging system, cameras, rovers, Mars, 1.2 Imaging System Design operations. The MER cameras are classified into five types: Descent cameras, Navigation cameras (Navcam), Hazard Avoidance 1 Introduction cameras (Hazcam), Panoramic cameras (Pancam), and Microscopic Imager (MI) cameras.
    [Show full text]
  • Of Curiosity in Gale Crater, and Other Landed Mars Missions
    44th Lunar and Planetary Science Conference (2013) 2534.pdf LOCALIZATION AND ‘CONTEXTUALIZATION’ OF CURIOSITY IN GALE CRATER, AND OTHER LANDED MARS MISSIONS. T. J. Parker1, M. C. Malin2, F. J. Calef1, R. G. Deen1, H. E. Gengl1, M. P. Golombek1, J. R. Hall1, O. Pariser1, M. Powell1, R. S. Sletten3, and the MSL Science Team. 1Jet Propulsion Labora- tory, California Inst of Technology ([email protected]), 2Malin Space Science Systems, San Diego, CA ([email protected] ), 3University of Washington, Seattle. Introduction: Localization is a process by which tactical updates are made to a mobile lander’s position on a planetary surface, and is used to aid in traverse and science investigation planning and very high- resolution map compilation. “Contextualization” is hereby defined as placement of localization infor- mation into a local, regional, and global context, by accurately localizing a landed vehicle, then placing the data acquired by that lander into context with orbiter data so that its geologic context can be better charac- terized and understood. Curiosity Landing Site Localization: The Curi- osity landing was the first Mars mission to benefit from the selection of a science-driven descent camera (both MER rovers employed engineering descent im- agers). Initial data downlinked after the landing fo- Fig 1: Portion of mosaic of MARDI EDL images. cused on rover health and Entry-Descent-Landing MARDI imaged the landing site and science target (EDL) performance. Front and rear Hazcam images regions in color. were also downloaded, along with a number of When is localization done? MARDI thumbnail images. The Hazcam images were After each drive for which Navcam stereo da- used primarily to determine the rover’s orientation by ta has been acquired post-drive and terrain meshes triangulation to the horizon.
    [Show full text]
  • The Mars Science Laboratory (Msl) Navigation Cameras (Navcams)
    42nd Lunar and Planetary Science Conference (2011) 2738.pdf THE MARS SCIENCE LABORATORY (MSL) NAVIGATION CAMERAS (NAVCAMS). J. N. Maki1, D. Thiessen1, A.Pourangi1, P. Kobzeff1, L. Scherr1, T. Elliott1, A. Dingizian1, Beverly St. Ange1, 1Jet Propulsion La- boratory/California Institute of Technology, 4800 Oak Grove Drive, Pasadena, CA 91109. Introduction: The Mars Science Laboratory (MSL) The camera plate, which also holds the Mastcam and Rover (scheduled for launch in November/December Chemcam instruments, is mounted to a 0.85-meter 2011) will fly four Navigation Cameras (Navcams). high Remote Sensing Mast (RSM), which points the The key requirements of the Navcam imaging system cameras in the azimuth and elevation directions. The are: 1) provide terrain context for traverse planning RSM is attached to the rover deck, which is 1.1 meters and Mastcam/Chemcam pointing, 2) provide a 360- above the nominal surface. The resultant configura- degree field of regard at <1 mrad/pixel angular resolu- tion places the Navcams 1.9 meters above the Martian tion, 3) provide stereo ranging data out to 100 m, and surface (0.4 meters higher than the MER Navcams). 4) use of a broadband, visible filter. The Navcams The MSL Navcams are build-to-print copies were built at the Jet Propulsion Laboratory in Pasade- of the Mars Exploration Rover (MER) cameras, which na, CA. are described in detail in [1]. The main difference Instrument Details: The mounting locations of the between the MER and MSL cameras is that the MSL Navcams are shown in figure 1. Navcams have slightly more powerful heaters to allow operation at colder ambient temperatures.
    [Show full text]
  • IMAGING from the INSIGHT LANDER, J. Maki1, A. Trebi-Ollennu1, B
    50th Lunar and Planetary Science Conference 2019 (LPI Contrib. No. 2132) 2176.pdf IMAGING FROM THE INSIGHT LANDER, J. Maki1, A. Trebi-Ollennu1, B. Banerdt1, C. Sorice1, P. Bailey1, O. Khan1, W. Kim1, K. Ali1, G. Lim1, R. Deen1, H. Abarca1, N. Ruoff1, G. Hollins1, P. Andres1, J. Hall1, and the InSight Operations Team1, 1Jet Propulsion Laboratory, California Institute of Technology (4800 Oak Grove Drive, Pasadena, CA 91109, [email protected]). Introduction: After landing in Elysium Planitia, Mars Table 1 gives a summary of the key camera characteris- on November 26th, 2018, the InSight mission [1] began tics. For a more detailed description of the InSight cam- returning image data from two color cameras: the In- eras, see [2]. strument Context Camera (ICC), mounted on the lander body underneath the top deck, and the Instrument De- ployment Camera (IDC) mounted on the robotic arm (Figure 1, [2], and [3]). Images from these color cam- eras have helped the mission meet several key objec- tives, including: 1) documentation of the state of the lander, robotic arm, and surrounding terrain, 2) terrain assessment for the selection of the SEIS [4] and HP3 [5] instrument deployment locations, 3) facilitation and documention of deployment activities, 4) monitoring of the state of the instruments post-deployment, and 5) monitoring of atmospheric dust opacity. The cameras are also providing information about the geologic his- tory and physical properties of the terrain around the lander [6,7,8,9]. Figure 2. First image acquired by the ICC. The trans- parent dust cover was in the closed position when this image was acquired.
    [Show full text]
  • A Multi-Resolution 3D Reconstruction Tool: Exemplar Using MSL Navcam PDS and Mastcam PIO Imagery
    EPSC Abstracts Vol. 8, EPSC2013-584-3, 2013 European Planetary Science Congress 2013 EEuropeaPn PlanetarSy Science CCongress c Author(s) 2013 A Multi-resolution 3D Reconstruction Tool: Exemplar using MSL NavCam PDS and MastCam PIO imagery Y. Tao, J.-P. Muller Imaging Group, Mullard Space Science Laboratory, Dept. of Space and Climate Physics, University College London, Holmbury St. Mary, Dorking, Surrey, RH56NT, UK ([email protected]; [email protected]) Abstract Based on the development work done during the PRoVisG project, we have extended our wide The acquisition of multi-resolution ground level baseline stereo reconstruction tool to be able to imaging data from different cameras onboard the produce multi-resolution 3D products via co- NASA MSL Curiosity, such as the Hazcams, registration of images from different cameras. In this Navcams, Mastcam and MAHLI, enable us to study a paper, we demonstrate this data fusion capability particular area/objects at various levels of detail. using the publicly released NavCam stereo PDS data However, to analyze the structural differences to provide 3D terrain context and co-registered properly or to do any extensive classification and MastCam images from the NASA Public Information recognition requires 3D information as well as the Office (PIO) website in order to reconstruct a high- 2D data from all of these cameras. This requires 3D resolution 3D colour model. reconstruction and co-registration of stereo rover and non-stereo rover imagery. 2. Methods In this paper, we describe the operation of a stereo We initially use the CAHVOR camera model stored reconstruction tool (StRec) with examples on 3D in the PDS header for intra-stereo reconstruction and ground reconstruction from both stereo and non- inter-stereo network building.
    [Show full text]