© 20 1 5 D JI . A l l Rights Re se rv e d . 

# Enoch Porter Fairbanks UAS Photography 303 Beaver Blvd. North Pole, AK 99705 January 7, 2016 I, Enoch Porter, hereb y s ubmit a petition for exemption under Section 333; FAA Modernization and Reform Act of 2012, Public L aw 112 - 95 FEB. 14, 2012, Section 333. Irequest exemption in order to operate m y DJ I f450 UAS with DJINAZA V2 flight controller and GPS . The manual for this UAS flight controller can be found here and will be fully copied below: http://dl.djicdn.com/downloads/nazam - v2/en/NAZA M_Quick_Start_Guide_v1.28_en.pdf My company will use this exemption, upon approval, to pr ovide and profit from services including aerial photograph y, aerial cinematograph y, aerial filming, photograph y for real estate, construction firms, agricultural modeling, crop monitoring operations, aerial mapping, special events to include but not limite d to weddings, private or public parties/events, business advertising, promotional events, geological surveying, and environmental studies. These services will provide safet y enhancements to Alaska residents and wildlife as well as a more cost effective me ans of obtaining aerial imagery for consumers. This petition was written with regard to approved petitions numbered: 12108, 11240, 11625, 11465, 14080, 14077, and 14085 Address of applicant: Enoch Porter Fairbanks UAS Photography 303 Beaver Blvd. North Pole, AK 99705 Phone: (907) 378 - 9851 Email: porterenoch52@gmail.com

Aircraft and Equivalent Level of Safety The high quality

DJ I NAZA V2 flight controller onboard the f450 UAS boast s all the safet y enhancing features found aboard the DJ I Inspire and DJI© 20 1 5 D JI . A l l Rights Re se rv e d . 

# Phantom series as well as the same advanced flight algorithms . The f450 is also the same size as a DJIPhantom and marginally lighter. If the UAS loses radio connection with the operat or it will rise to a predetermined safe elevation and fl y back to where it took off. If the battery power falls below a DJIrecommended level the UAS will also return to the home point in the same fashion. The UAS altimeter is set to prevent the UAS from traveling over 200 feet. The f450 UAS weighs under 15 pounds and an y change in sensor payload or camera will be noted in the log book, tested in a safe area, and kept under 15 pounds. The operator will fly under normal conditions at a speed of no more than 35 knots and have the c apability to hover and move in the vertical and horizontal plane simultaneously . The operator will manually operate onl y in visual line of sight and will operate only within the confined areas described herein. Giv en the small size and weight of the UAS involved and the restricted sterile environment with in which it will operate, Fairbanks UAS Photograph y falls squarely within that zone of safety (an equiv alent level of safet y) in which Congress envisioned that the FAA, by exemption , allows c ommercial operations of UASs to commence. Also due to the size of the UASs and the restricted areas in which the relevant UAS will operate, approval of the application presents no national security issue. Fairbanks UAS Photography will alway s be bound to following these limitations and conditions when conducting commercial operations under section 333 exemption. 1. The UAS will weigh less than 15 lbs when carrying a load, is constructed by a high reputati on company and uses a Multi - copter base application. 2. Flights will be operated manually within visual line of sight (VLOS) of the Operator (PI C) and Observers 3. Maximum total flight time for each operational flight will depend on battery charge, the ave rage flight will be 30 +/ - minutes. Flights will be terminated at 25% battery power reserve should that occur prior to the 30 +/ - minute limit. 4. Flights will be operated at an altitude of no more than 200 feet AGL. The DJINaza V2 flight controller has b een programmed to fly no higher than 200 feet. 5. Minimum two (2) man crew for each UAS operation will consist of the Operator and Observer.© 20 1 5 D JI . A l l Rights Re se rv e d . 

# 6. The UAS will only

operate within a confined and controlled privatel y owned area with owner written permission, or with permission from local government in public arias. 7. Fairbanks UAS Photograph y will use procedures to document and maintain records of the UAS maintenance, preventative maintenance, alteration records, and status of replacement/overhaul component parts. 8. A pre - flight safet y risk assessment procedure, according to the manual, and a briefing will be conducted in regard to the planned UAS operation prior to each day ’s production activities. It will be mandatory that all personnel who will be perform ing duties within the boundaries of the safety perimeter be present for this briefing. 9. Spotter (Observer) and Operator will at all times be able to communicate by voice. 10. All required permissions and permits will be obtained from state, county or city jurisdictions. 11. If the UAS loses communications or loses its GPS signal, the UAS will have capability

to return to a pre - determined location within the Security Perimeter and land. 12. The UAS will have the capability to abort a flight in case of unpr edicted obstacles or emergencies. 13. The UAS will not be operated less than 500 feet below or less than 2,000 feet horizontally

from a cloud or when visibility is less than 3 statute miles from the PI C. 14. The PI C will have an aviation sport license. PIC will have training on the specific manual to the UAS and a minimum of 7 hours or ten 30 minute practice runs with the specific UAS following our guidelines for operation pursuant to this petition. 15. UAs will never come within range of power lines, light poles, airports, heavily populated areas, or any

other environment which may cause accidents. Only under these conditions will the UAS operate.

Extent of Relief Exemptions list The requests of this petition are similar to those of Brian Punch, Mr. Jas e W. Robak, Mr. Todd Thomas of Drone Pics, Brandon Drivon, Mr. Mike Llo yd Llo yd & Associates, Mr. Scott vigneault of Birds Ey e View, and Mr. Brent Van Palmer, all of whom have received Section 333 exemptions for© 20 1 5 D JI . A l l Rights Re se rv e d . 

# comparable aircraft for similar operations. The specific sections of 14 C.F.R from which I am seeking exemption are as follows: 14 C.F.R. Part 21; 14 C.F.R. 45.23(b); 14 C.F.R. 61.101(e)(4), & (5); 14 C.F.R. 61.113(a) & (b); 14 C.F.R. 61.133 (a); 14 C.F.R. 61.23(a) & (c); 14 C.F.R. 61.315 (c) (2) & (3); 14 C.F.R 91.7(a) 14 C.F.R. 91.9(b)(2); 14 C.F.R. 91.103; 14 C.F.R. 91.109(a); 14 C.F.R. 91.119; 14 C.F.R. 91.121; 14 C.F.R. 91.151(a); 14 C.F.R. 91.203(a) & (b); 14 C.F.R. 91.405(a); 14 C.F.R. 91.407(a)(1); 14 C.F.R. 91.409(a) (2); 14 C.F.R. 91.417 (a)&(b); Extent of relief requested This request is submitted in accordance with the Reform Act, 112 P.L. 95 §§ 331 - 334, seeking relief from any currently applicable FARs, operating to prevent one from producing commercial flight operations within the n ational airspace sy stem. The Reform Act in Section 332 provides for such integration of civil unmanned aircraft s ys tems into our national airspace sy stem as it is in the public's interest to do so. Fairbanks UAS Photography’s DJIf450 meets the definition of "Small Unmanned Aircraft" as defined in Section 331 and therefore the integration of this ultra light weight UAS is expressly contemplate d by

the Reform Act. Fairbanks UAS Photography will supply aerial photography , aerial cinematograph y, aerial filmin g, photograph y for real estate, construction firms, agricultural modeling, crop monitoring operations, aerial mapping, special events to include but not limited to weddings, private or public parties/events, business advertising, promotional events, geolog ical surveying, and environmental services.© 20 1 5 D JI . A l l Rights Re se rv e d . 

# Fairbanks UAS Photography cannot sustain itself without obtaining profit from its customers; therefore an exemption is required from the above mentioned 14 C.F.Rs. Social Benefit Within these exemptions, comme rciall y fl yi ng this UAS for reality , cinematograph y, and aerial photograph y will reduce danger b y keepi ng large fixed wing aircraft far from delicate Alaskan ecos ystems where exhaust and noise are harmful and the danger of a high explosive crash are fatal. The ultra light electric UASs pose no threat to the wildlife and are quite enough to be ignored b y animals and local residents. In the reality business especiall y aerial footage can be brought to a reasonable price for the regular consumer through UAS int egration. As there are many military personnel constantly

moving in and out of bases in Alaska this is a need which must be satisfied. Alaska’s economy is largel y based on tourism which could equally benefit from fair priced aerial photograph y.

Summary for Federal Register A. 14 C.F.R. 21 and 14 C.F.R. 91: Airworthiness Certificates, Manuals and the like. 14 C.F.R. 21, Subpart H, entitled Airworthiness Certificates, sets forth requirements for procurement of necessary airworthiness certificates in relation to FAR § 91.203 (a) (1). The size, weight and enclosed operations area of m y UAS permits exemption from Part 21 because m y UAS meets an equivalent level of safet y pursuant to Section 333 of the Reform Act. The FAA is authorized to exempt aircraft from the airworthiness certificate requirement under both the Act (49 U.S.C. § 44701 (f) and Section 333 of the Reform Act. Both pieces of legis lation permit the FAA to exempt UAS's from the airworthiness certificate requirement in consideration of the wei ght, size, speed, maneuverability and proximity

to areas such as airports and dense populations. The UAS in question meets or exceeds each of the elements. 14 C.F.R. 91.7 (a) prohibits the operation of an aircraft without an a irworthiness certificate. As n o such certificate will be applicable in the form contemplated b y the FARs, this Regulation is inapplicable. 14 C.F.R. § 91.9 (b) (2) requires an aircraft flight manual in the aircraft. As there are no pilots or p assengers and given the size of the UAS, th is Regulation is inapplicable.© 20 1 5 D JI . A l l Rights Re se rv e d . 

# An equivalent level of safety will be achieved b y maintaining a manual. The FAA has previousl y issued exemptions to this regulation in Exemption Nos. 8607, 8737, 8738, 9299, 9299A, 9565, 9565B, 10167, maintenance program that involves regular software updates and c urative measures for an y damaged hardware. Therefore, an equivalent level of safet y will be achieved. Respectfully ,

Enoch Porter Fairbanks UAS Photography 303 Beaver Blvd. North Pole, AK 99705 Phone: (907) 378 - 9851 Email: porterenoch52@gmail.com© 20 1 5 D JI . A l l Rights Re se rv e d .



# Naza - M V2 Q u i ck S t art Gu i d e V 1 . 2 8

2 0 1 5 . 0 6 .1 2 Re v i s i o n F o r 

### F ir m w a r e V e r s i o n V 4 . 0 4 o r 

### ab o v e & A ss i s ta nt S o f

t w a re 

### V e r s i o n V2 . 4 0 o r ab o v e

T h ank yo u f

o r pur c h a s i ng t

h i s DJI p ro du c t . Ple a s e s t ri c tl y f o ll o w t he s e s t eps t

o m o unt and c o nne ct t

h i s s y s t em o n yo ur a i r c r a f

t , a s w ell a s t o in s ta ll t

he A ss i s ta nt S o f

t w a re o n yo ur c o m

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## * a t o ur w eb s i t e 

## w ww. d ji . c o m , wh i ch i s upd a t ed re g ul a rl y . P r o d

u c t in f o rm a ti o n, te c hn i c a l upd at es and m a nu a l c o rr e c ti o ns w ill be a v a i l a b l e o n t h i s w eb p a g e. Due t o un f

o re s een c h a n g es o r p r o du c t up gr a de s , t he in f o r m a ti o n c o nt a i ned in t h i s m a nu a l is s ubje c t to c h ange w i th o u t n o ti c e . 

## * I m p o rta nt : N a z a - M, N a z a - M V2 and P HAN T OM c o nt r o l s y s t e m a re di f f erent in h a r dwa re p ar t s , b u t t h e i r c o n f i g ur a ti o ns a nd f

un c ti o ns a re t

h e s am e w

hen u s i ng t

he s am e A ss i s ta nt S o f

t w a re and F irm w a re V e r s i o n, s o t hey u s e t he s a m e Gu i de. U nle s s s t a ted, t he f o ll o w i ng in s t

ru c ti o n is b a s i c o n N a z a -M V 2 . I f yo u u s e t he N a z a - M, p l e a s e m a ke s ure t o re a d t

he “ I n s t ru c ti o n o f V 1 ( a l s o k

n o wn a s N a za - M ) ” s e c ti o n ; if y o u u s e t he P HAN T OM, d o wnl oa d t h e o t her c o r r e s p o nding m a nu a l s o n t he P HA N T OM w e b p a g e . T h i s m a nu a l is o nly f

o r b a s i c a ss e m

b ly a nd c o n f

i g ur a ti o n; yo u c a n o b ta in m o re de ta i ls a nd a dvan c ed in s tru c ti o ns when u s i ng t

he a ss i s ta nt s o f

tw a r e . T o a ss ure yo u h a v e t he l a t e s t in f

o rm a ti o n, p le a s e v i s i t o ur w eb s i te a nd d o wn l o a d t he l a t e s t m a nu a l and cu rr ent s o f t w a re v er s i o n. I f y o u h a ve a ny p r o b l em t h a t yo u c ann o t s o lve dur i ng u s a g e, p l e a s e c o n t a ct yo ur aut h o ri z ed de a ler .© 20 1 5 D JI . A l l Rights Re se rv e d . 

# I nd e x I N DE X **............................................................................................................................. .................................................**  **. 2**  I N S T RU C T I ON **............................................................................................................................. ...................................**  **. 3**  D I SC L A I M E R & W A R NIN G ............................... . ............................... . ............................... . ............................... . ................... . 3 T R AD E M A R K ............................... . ............................... . ............................... . ............................... . ............................... . .... . 4 C E R TI F I C A

TI O N S ............................... . ............................... . ............................... . ............................... . ............................... . . 4 S Y M BO L I N S T R U CTI O N ............................... . ............................... . ............................... . ............................... . ........................ . 4 A S S EM B L Y & C O N N E C T I O N **............................................................................................................................. ..........**  **. 5**  S TE P 1 P OR T D E SC R I PT I O N ............................... . ............................... . ............................... . ............................... . .................. . 5 S TE P 2 A SS E M B L

Y & C O NNE CTI O N ............................... . ............................... . ............................... . ............................... . ........ . 6 A S S I S T A NT S O FT W ARE I N S T AL LA T I ON A ND C O N F I GU RA T I ON **........................................................................... .**  **7** S TE P 1 S O F T W

A R E A N D D R I V E R I N S T

A L L A TI O N ............................... . ............................... . ............................... . ......................... . 7 S TE P 2 C O N F I G U R A

TI O N B Y A SS I S T

A N T O N A PC ............................... . ............................... . ............................... . ....................... . 8 B A S I C F L Y I N G **............................................................................................................................. .................................**  **. 10**  C O NT R O L M O D E K N O W L E D G E ............................... . ............................... . ............................... . ............................... . ........... . 10 S T A R T & S T O P M O T O R K N O W L E D G E ............................... . ............................... . ............................... . ............................... . ... . 10 S TE P 1 C O M P

AS S C A L I BR A

TI O N ............................... . ............................... . ............................... . ............................... . ........... . 12 S TE P 2 A SS E M B L

Y C H E C K IN G L I S T ............................... . ............................... . ............................... . ............................... . ........ . 13 S TE P 3 B E F OR E F L I G H T ............................... . ............................... . ............................... . ............................... . ..................... . 13 S TE P 4 F L YIN G T E ST ............................... . ............................... . ............................... . ............................... . .......................... . 14 A D V AN C ED F UN C T I O N S **............................................................................................................................. ..............**  **. 16**  A1 F A I L S A F E ............................... . ............................... . ............................... . ............................... . ............................... . .. . 16 A2 LO W- V O L

T A G E A L E R T ............................... . ............................... . ............................... . ............................... . .................. . 17 A3 I NTE LL I G EN T O R IEN T A TI O N C O NT R O L ( I O C ) F L I G H T ( WIT H G PS M O D U L E ) ............................... . ............................... . .............. . 18 A4 R E C EIVE R A D V

A N C E D P R O TE CTI O N F U N CTI O N ............................... . ............................... . ............................... . .................. . 21 A5 F L I G H T L I M IT S ............................... . ............................... . ............................... . ............................... . ........................... . 22 A PPE N D I X **............................................................................................................................. .......................................**  **. 23**  S P E C I F I C A

TI O N S ............................... . ............................... . ............................... . ............................... . .............................. . 23 MC /P M U F I R M W

A R E U P G R AD E ............................... . ............................... . ............................... . ............................... . ....... . 24 L E D D E SC R I PT I O N ............................... . ............................... . ............................... . ............................... . ........................... . 25 I N S T RU C T I ON OF V 1 **(** A L S O K N O W N A S N AZ A - M ) **................................................................................................. .**  **26** V 1 A SS E M B L

Y A N D C O NNE C TI O N ............................... . ............................... . ............................... . ............................... . ........ . 26 V 1 I S C O M P

A TI BL E WIT H T H E P M U V 2 ( A CC E SS OR Y O F N A Z A - M V 2 ) ............................... . ............................... . ........................ . 26 V 1 P O R T D E SC R I PT I O N ............................... . ............................... . ............................... . ............................... . ..................... . 27 V 1 S P E C I F I C A

TI O N ............................... . ............................... . ............................... . ............................... . ........................... . 28 F A Q **............................................................................................................................. ..................................................**  **. 29**  A B N OR MA L L E D I N D I C A TI O N L I S T ............................... . ............................... . ............................... . ............................... . ....... . 29 F I X T H E TBE ( T O I L E T B O W L E FF E CT ) P ROBL E M ............................... . ............................... . ............................... . ...................... . 29 S HO U L D Y

O U F IN D T H E MU L

TI - R O T O R D O E S N O T T R AC K S T R A I G H T I N F OR W A R D F L I G H T. ............................... . ............................... . .. . 30 M O T OR S S T A R T FA I L U R E CA U S E D B Y TX S T I C K ( S ) M I D - P O IN T E RRO R T O O B I G ............................... . ............................... . ................ . 30 A TTIT U D E C O NT RO L L A BL E W H E N O N E M O T O R O U T P U T I S F

A I L E D ............................... . ............................... . ............................. . 31 W H E N U S E D WIT H O T H E R DJI P R O D U CT S ............................... . ............................... . ............................... . ............................. . 31© 20 1 5 D JI . A l l Rights Re se rv e d . 

### 3 | 

# I n s t r u c tion D i s c l a im er & W ar

n in g P l e a s e re ad 

### th i s d i 

### s c l a i me r c a r e f ul ly b e f ore 

### u s in g th e 

### p r o du c t . B y 

### u s in g t h i s pr o d u c t , y o u 

### h e r e by agre e t o 

### t

h i s d i s c l a i me r a

n d 

### s i g n i fy t h a t y ou h av e re ad t

h em 

### f u l l y . T H IS P R

O DU C T 

### I S N O T SU I T A B LE F O R PE O PL E 

### U ND ER T H E AGE O F 

### 1 8 . T h i s p r o du c t is an aut o pil o t s y s t em de s i g ned f o r s eri o us m

ul ti - r o t o r en t

hu s i a s t s p ro v i ding e x c ellent s el f - le veling a nd a l ti t ude h o l d i ng , wh i c h c o m p l e tely t a kes t

h e s t re s s o ut o f f

l ying R C m

ul ti - r o to rs f

o r b o t h p ro f e s s i o n a l a nd h o b b y ap p li c a ti o n s . De s pi t e t

he s ys t em h a v i ng a buil t - in au t o pil o t s y s t e m and o ur e ff o rt s in m a ki ng t he o pe r a ti o n o f t he c o nt r o ll er a s s a f

e a s p o ss i b l e when t

he m a in p o w er b attery is c o nne c te d , w e s t r o ngly re c o mm e nd u s ers t o re mo v e a ll p r o pe l lers w

hen c a libr a tin g a nd s e t

ti ng p ar a m e ter s . M a ke s ure a ll c o nn e c t i o ns a re g oo d, and keep c h i l d ren a n d a n i m a ls a wa y dur i ng f

i r mw a re up gr a de, s y s t em c a libr a ti o n a nd p ara m et er s e tup. DJI I nn o v a ti o ns ac c ep t s no li abili ty f o r d am a g e( s ) o r in

j uries in c urr ed dire c tly o r i ndire c t ly f r o m t he u s e o f t

h i s p r o du c t in t

h e f o ll o w i ng c o ndi t i o n s : 1 . D am a g e( s ) o r in

j uries in c urr ed when u s ers a re dr unk , ta ki ng dr

ug s , dr ug a ne s the s i a , di z z i ne s s , f a ti g ue, n a u s ea a nd a ny o t

her c o ndi t i o ns no m atter p h y s i c a l l y o r m ent a l l y t h at c o ul d i m

p a i r yo ur abili ty . 2 . D am a g e( s ) o r in

j uries c au s ed by s ubje c ti v e i nt ent i o n a l o pe r a ti o n s . Any m en t a l d am a g e c o m pen s a ti o n c a u s ed by a cc i d en t . 3. F a i lur e t o f

o ll o w t he gui d a n c e o f t he m a nu a l t o a ss e m

b l e o r o p e r a te. 4 . M a lf

un c ti o ns c au s ed by ref

i t o r rep l a c e m ent w i t

h n o n - DJI ac c e ss o ries and p a rt s . 5. D ama g e( s ) o r in

j uries c au s ed by u s i ng t

h i rd p art y p r o du c t s o r f

a ke DJI p ro du c t s . 6 . D ama g e( s ) o r in

j uries c au s ed by mi s - o pe r a ti o n o r s ubje c ti v e mi s - j ud g m ent . 7. D ama g e( s ) o r in

j uries c au s ed by m e c h a n i c a l f a i lur es due t o ero s i o n, a g i ng . 8 . D am a g e( s ) o r in

j uries c au s ed by c o nti nued f l y ing a f t er l o w v o l t a g e p r o te c ti o n a l a rm is t rig g ere d . 9 . D am a g e( s ) o r in

j uries c au s ed by k

n o w i ng ly f

lyin g t he a i r c r a f

t in a bn o rm a l c o ndi t i o n ( s u ch a s w at er , o il, s o i l, s a nd and o t

her unk n o w n m a teri a l i ngre s s i nto t he a i r c r a f

t o r t he a ss em

b ly is n o t c o m

p l e te d , t he m a in c o m p o nen t s h a v e o b vi o us f

a ul t s , o b v i o us defe ct o r mi ss i ng a cc e s s o rie s ). 1 0. D am a g e( s ) o r in

j uries c au s ed by f

l y ing in t he f o ll o w i ng s i t

u a ti o ns s u c h a s t he a i r c r a f t in m a g ne t i c i nt erfere n c e a re a , r a dio i nt erferen c e a re a , g o v e rnm e nt re g u l a t ed n o - f

ly z o nes o r t

he pil o t is in b a c klig h t , b l oc ked, f uz z y s i g ht , a nd p oo r e y e s i g ht is n o t s u i t ab l e f o r o pe r a ti ng a nd o t

her c o ndi t i o ns n o t s u i t ab l e f o r o pe r a ti ng . 11 . D am a g e( s ) o r in

j uries c au s ed by u s i ng in b a d w e a t her, s u ch a s a r a iny d ay o r w indy ( m o re t h an m o de r a te b r eeze ) , s n o w , h a il, lightn i ng , t o rn a d o e s , hurr i c a nes e t c . 1 2 . D am a g e( s ) o r in

j uries c au s ed w

h en t he a i r c r a f

t is in t he f

o ll o w i ng s i t

u a ti o n s : c o ll i s i o n, f

i r e, e x p l o s i o n, f

l o o d s , t s un a m i s , s ub s i den c e, i c e t r ap p ed, a v a l a n c he, deb ris f l o w , l a nd s lid e , e a r

t hqu a k e, e tc . 1 3. D am a g e( s ) o r in

j uries c au s ed by in f

ringe m ent s u c h a s any da ta , audio o r v i deo m a t eri a l re c o rd ed by t he u s e o f a i r c r a f t . 1 4 . D am a g e( s ) o r in

j uries c au s e d by t

he mi s u s e o f t

he b a tt e ry , p ro te c ti o n c i r c u i t , R C m o del and b att ery c h a rg er s . 1 5. O t her l o ss es t

h at a re n o t c o v ered b y t

he s c o pe o f DJI I nn o v a ti o ns li abili ty .© 20 1 5 D JI . A l l Rights Re se rv e d . 

### 4 | 

## T ra d e m ark DJI a nd N a z a - M a re re g i s t ered t r a dem ar ks o f DJI I nn o v a ti o n s . N a m es o f p r o du c t , b r and, e t c . , ap p e a ring in t h i s m a nu a l a re t

r a dem ar ks o r re g i s tered t r a dem ar ks o f t

he i r re s pe c ti v e o wn e r c o m p a n i e s . T h i s p r o d

u ct a nd m a nu a l a re c o p y righ ted by D J I I nn o v a ti o ns w i t h a ll righ t s re s erve d. No p art o f t h i s p r o du c t o r m a nu a l s h a ll be re p r o du c ed in a ny f o rm w i t h o ut t he p ri o r wri tten c o n s en t o r a ut h o ri z a ti o n o f DJI I nn o v a ti on s . No p at ent li abili ty is a ss um ed w i th re s pe ct t o t

he u s e o f t

he p r o du ct o r in f

o rm a ti o n c o n ta i ned herein. 

## C e rt i f i c a t i o n s T h i s p r o du c t i s ap p r o v ed w i t h qu a li t y s ta nd ard s s u ch a s C E, F C C and R o H S . 

## S ymb o l I n s t

r u c ti o n F o r b i d d en( I mp o rta n t) C a uti o ns T ip R e f eren c e© 20 1 5 D JI . A l l Rights Re se rv e d . 

### 5 | T: For throttle control R: For rudder control U: For Control Model Switch X1: For gimbal pitch control / F X2: For D - Bus(S - Bus/S - Bus2 c X3: For voltage monitor(Conne

M1: M2: M3: M4: M5: M6: F1: T F2: T NAZ

Extended CAN port EXP : Connec t t o Mai n Controller EXP port 

# A s s emb ly & C o nn e c t ion I n t he B o x : M a in c o nt

r o ll er X 1 , PMU X 1 , G P S X 1 , G P S B r a c k et X 1 , L ED X 1 , S e rvo C ab l e X 8 , M i c r o - U S B C ab l e X 1 , 3M A dhe s i v e T ape . 

## S t e p 1 P o rt D e s c r i pt i o n

EXP:Connect to PMU module LED:Connect to LED module A: For roll control (left/right) E: For pitch control (front/back)

or gain tuning om patible) / For gain tuning / F or IOC swi t ch ct to PMU V - SEN port) Pointing to the aircraft nose direction



### Main **C o**  **n t**  **r o**  **ll e**  **r** To #1 ESC(*) To #2 ESC To #3 ESC To #4 ESC To #5 ESC To #6 ESC o gimbal roll servo or To #7 ESC o gimbal pitch servo or To #8 ESC A output is 400Hz refresh frequency V - SEN: Connect to Main Controller X3Port **Important** : the continuous output of the PMU is 3A@5V, and the maximum instant current is 7.5A. If PMU cannot afford the working current for your servos, please use an independent power supply; otherwise, it ma y cause the PMU safeguard and lead to the main controller reboot 。 

### Ma **in** 

### Contro **ll er** 

**PMU** (Power Management Uni t )

2S~6S: Powered by 2S~6S LiPo(7.4V~26.0V)

GPS: Connect to GPS/Compass module

Connect to Main Controller LED port

Micro - USB : P C connectio n for parameter configuration and firmware upgrade 

### LED Pointing to the aircraft nose direction Connect to GPS port of PMU 

### GPS **/ Compass**  *ESC: Electronic Speed Con t roller© 20 1 5 D JI . A l l Rights Re se rv e d . 

### 6 | gummed paper pro

**)** h e d e r **PMU Module**  a 3 - **Mount** : D O NO T attac h th e PM U othe r device . Sufficien t ai r flo w o

**A ILE**  **ELEV (JR)**  **T HR**  **O**

**RUDD 3**  **- position**  **Swi tc**  **h A**  **E T**  **MC R**  **U 1**  **(Futaba 2**  **/Hitec) 3**  **3 -**  **position Switch**  **A E**  **T MC**  **R U**  

## S te p 2 A ss e mb ly & C o nn e c t i o n Step1 Prepare an aircraft, su pported th e following **Mixed Types**  . The direction of the arrow in diagram indicates the rotation direction of the mo t or / propeller . **Important** : To coaxial propellers: Blue propeller is at TOP ; Red propeller is at Bottom . Otherwise all propellers are at t op .

**Quad -**  **rotor I**  **Quad -**  **rotor X**  **Hexa -**  **rotor I**  **Hexa -**  **rotor V**  **Hexa -**  **rotor I**  **Y ESC**  **& MC**  **Connection**

**Hexa -**  **rotor Y**  **Octo -**  **rotor I**  **Octo -**  **rotor V**  **Octo -**  **rotor X**  **A i**  **rcraft M1**  **M2 M3**  **M4 M5**  **M6 M7**  **M8 Main**  **C on**  **tr oll**  **er**

**M1 M2**  **M3 M4**  **M5 M6**  **F 1**  **F 2**  N o t e : The NAZA - M V2 f li g ht c o ntr o l system doesn't support Gimbal f un c t i o n when used on the Octo - rotor a i r c r a f t . For b i g a i r c r a f

t that is l ar g e r than 650 or with heavy l o a d , WKM is r e c o mm e n d e d . Step2 Assembly and Connection

**Main C**  **on tr** **oll er(MC)**  **Mount** : (1)Th e DJ I log o shoul d fac e th e sky , DO NOT mount the MC upside - dow n . (2) The MC sides should be parallel to the aircraft body. (3)Th e arro w shoul d poin t t o th e nos e directio n o f aircraft
. (4) he MC is best positioned near the a i r c r a f t ’s center o f gravity. Make sure all ports are accessible . **T i**  **p** : It is recommended to f i x the MC until all wirings and configurations are complete d , u sin g 3M

vided to fix the MC
. **ESCs &**  **Motors** Pleas e us e th e ESC s an d motors recommende d b y th e manu f ac t ure r of your aircraft. We recommend you use DJI motors and ESCs (Re f er t o it s manua l fo r details)
. Connec t al l ESC s t o M C b y th e mo t o r numbering method introduced in mixed types Supported . **Important** : I f yo u us e 3r d part y ESCs , mak e sur e th e ESC s t rave l midpoin t i s a t 1520us . D O NO T us e 700u s trave l midpoin t ESC , a s i t ma y lea d aircraft t o fl y awa y o r caus e injur y an d damage . Afte r ESC s connectio n , calibrat e ESC s on e b y on e throug h th e receive r direc t l y before connec t the m t o you r MC , Mak e sure progra m al l o f the m in t o Governor off, Break off and Normal Start up to get best experience . **Traditional Receiver**  **S -**  **Bus/S -**  **Bus2/PPM Receiver**  **ESCs Gimbal**  Connec t th e gimba l servo s t o t h e p o r t s o f F 1 a n d F 2 i f a gimba l i s used , an d us e t h e software for con f igura t ions .

**F2 Power**  **Supply** R o ll P i t c h **Transmitter(TX) &**  **Receiver(RX** ( 1 ) R e f e r t o y o u T X M a n u a l , s e t u p t A i l e r o n , E l e v a t o r , T h r o t t l e , R u d channels on your TX first, and choose position switch as control mode swi t ch . (2)Attach the matched RX to aircraft, t hen the PMU is highly recommended . o n ve r **F1**

**(Optional)GPS/Compass Mount**  : GPS/Compass is sensitive t o magnetic interference, should be f ar away from any electronic devices. If you use your own mounting rod , make sure it is NOT magne t ic ! **Procedures** : connect your RX to the right ports on MC
. The following diagram shows t he connection example for traditional RX .

**4** Step3 Double Check **Tip** : I f us e wit h DJ I multi - rotor , yo u ca n solde r th e powe r cabl e t o powe r pad s o n fram e botto m board . Pleas e refe r t o DJ I multi - roto r manua l f o r details . I f us e wit h 3r d par t aircra ft , y o u c a n m a k e a c o n n e c t e r b y yourself to connect PMU and ba tt ery . **LED Module**  **Mount** : M ake sure Yo u ca n se e th e ligh t durin g t h e f ligh t . Leav e th e US B interfac e t o b e accessible . Us e th e 3M gummed paper provided to f ix . (1)Yo u shoul d us e epox y resi n A B glu e t o assembl e th e GP S bracke t f irs t . Moun t t h e bracke t o n t h e cen t e r pla t e o f cra ft . P o s i t io n t h e b ra ck e t a t least 10 cm from any propeller . (2)Th e DJ I log o marke d o n th e GP S s h o u l d f a c e t h e s k y , w i t h t h e orientatio n arro w pointin g direc t l y forward
. the n fi x th e GP S o n th e pla t e of the bracket (by 3M glue provided)
. **Ti p**  : Th e GPS/Compas s i s package d w i t h a s p e c i a l i n d i c a t i o n l i n e f o r mounting for the first t ime . In th i s s t e p , turn on the tr a n s m i tt e r , connect the battery to the PMU, and then watch the LED, if you can see the LED b li nk s ( ), the system is w o rk i n g .© 20 1 5 D JI . A l l Rights Re se rv e d . 

### 7 | 

# A ss i s tan t S o ftw ar e In s t a l l ati o n and Con f i gur a tion S t e p 1 S o f tw ar e a n d D ri v e r I n s t a ll a

t i o n I n s ta ll i ng a nd runn i ng o n W i nd o w s 1 . Ple a s e d o w

nl oa d t he dri v er a nd t

he Assis tant in s ta ll a ti o n s o f t w a re in E X E f

o rm a t f r o m www . dj i . c o m . 2 . S w i t c h o n t

he t r a n s mi t t er a nd t hen p o w er o n yo ur aut o pil o t s y s t e m . 3. C o nne c t yo ur aut o pil o t s y s t e m and PC v ia a M i c r o - U S B c a b l e . 4 . Open t

he dri v er in s ta ll a ti o n s o f

t w a re and f

o ll o w t he in s t ru c ti o ns t o c o m

p l e t e in s ta ll a ti o n . 5. R un t he A ss i s ta nt in s ta ll a ti o n s o f t w a re a nd f

o ll o w t he in s tr u c ti o ns t o c o m

p l e t e in s ta ll a ti o n . T he in s ta ll er in E X E f

o rm a t is s upp o r

t ed o n W i n X P, W i n7, W i n8 (32 o r 6 4 bi t) . I n s ta ll i ng a nd runn i ng o n M a c O S X 1 . D o w

nl oa d t he A ss i s ta nt in s ta ll er i n DMG f o rm a t f r o m t h e d o w nl oa d p a g e o f NAZ A - M V2 o n t he DJI w eb s i te. 2 . R un t he in s ta ll a ti o n s o f

t w a re and f

o ll o w t he p r o m p t s t o f in i s h in s ta ll a ti o n.

3. When l aun ch i ng f o r t he f i r s t ti m e if u s e Laun c hp ad t o run t he N AZ A - M V2 A ss i s ta nt S o f t w a re, L a un c hp a d w o n ’ t a l l o w a cc e s s be c au s e t he s o f t w a re h a s n o t been re v i e w ed by M a c A pp S to re.© 20 1 5 D JI . A l l Rights Re se rv e d . 

### 8 | 4 . Lo c a t e t

he N AZA - M V2 i c o n in t he F i nder a nd o pen t

he f i le by C o nt

r o l o r right c l i c k

i ng t he i c o n a nd s ele c ti ng “ Op en” f

r o m t he m enu . 5. A f t er t h e f i r s t s u cc e ssf

ul l aun ch, d o ubl e - c li c ki ng t he N A Z A - M V2 i c o n in t

he F i nder o r u s i ng L a un c hp a d w ill o pen t

he ap p li c a ti o n.

I n s ta ll er in DMG f

o rm a t is s upp o r

t ed o n M a c O S X 1 0 . 6 o r ab o v e. T he NA Z A - M V2 A ss i s ta nt o n M a c OS X and W i nd o w s a re e x a c tl y t h e s a m e. T he A ss i s ta nt ap pe ar in o t her p l a c es o f t

h i s m a nu a l is b as ed o n W i nd o w s v er s i o n. 

## S te p 2 C o n f

i gur at i o n b y A s s i s t an t o n a P C 1 . P o w er o n t

he P C . M a ke s ure yo ur c o m p u t er is c o nn e ct ed t o t

he I nt e rnet f

o r t h e f i r s t t i m e yo u u s e. 2 . S w i t c h o n t

he t r a n s mi tter f

i r s t , a nd t hen p o w er o n t he aut o pil o t s y s t e m . C o nn e c t t he aut o pil o t s y s tem to t he PC w i t

h a M i cr o - U S B c ab l e. DO NOT b r e a k t he c o nn e c ti o n un ti l s e t

up is f in i s hed. 3. R un t he A ss i s ta nt S o f

t w a re. 4 . Ob s erve t

he i ndi c a to rs o n t

h e left b o tto m o f t

he s o f t w are. ( They a re t

he c o n ne c ti o n i nd i c a to r a nd c o m m un i c a ti o n in di c a to r in o r d er . ) I f t he c o mm un i c a ti o n i ndi c a to r is b l in ki ng , t h a t t he s o f t w a re is re a d y , p l e a s e g o t o ne x t s tep. 5. S ele c t t

he “ In f o ” o p ti o n. C h e c k t

he s o f t w a re f irm w a re v e r s i o n. I f t

he up gra de i s a v a i l a b l e, yo u m a y upd a t e t he a ss i s ta nt s o f

t w a re.© 20 1 5 D JI . A l l Rights Re se rv e d . 

### 9 | 6 . S ele c t t

he “Up g r ade” o p ti o n. C h e c k t he M a in C o nt

r o l l e r, G P S and I MU f

irmw a re v er s i o n. 7. S ele c t the “ B a s i c ” o p ti o n. P l e a s e f o l l o w s t e p - b y - s t ep f

o r yo ur f i r s t - ti m e - c o n f

i g ur a ti o n. B a s i c c o n f

i g ur a ti o n is ne c e s s a ry , in c lud in g M i x er T y p e , M o un ti ng , R C , a nd G a in s e tti ng s . 8 . Y o u c an c li c k t

he “A dva n c ed” o p t

i o n f o r m o re p a

r am e t er s e t ti ng s . A d v a n c e d s e tti ng is o p t i o n a l. T he r e a re s e t ti ng s o f M o t o r, F a i l S a f

e, I nt e ll i g e n t Orie n ta ti o n C o nt r o l ( IO C ), Gi m b a l, L o w - Vo l t a g e A le r t , a nd F ligh t L i m i t s . R e a d t

he in s t r u c ti o n in t

he a ss i s t a nt s o f

t w a re t o o b ta in m o re de ta i l s . 9 . S ele c t t

he “ V ie w e r ” o p ti o n t o c he c k a ll p a r a m e t e r s . 1 0. Then b re a k t

h e M i c r o - U S B c a b l e , p o w er o f f t he a i r c r a f t . F i n i s he d . (1) Y o u ma y be re q

u i red t o f ill re g i s t e r i n f

o rm a ti o n f

o r yo ur f i r s t - ti m e - u s a g e . ( 2 ) I f t he c o m m un i c a ti o n indi c a to r is b lue o n, p l e a s e d o uble ch e c k t h e c o nn e c ti o n s . (3) B a s i c c o n f

i g ur a ti o n is ne c e ss a ry bef o re yo u g o t o t

he “ B a s ic F lyi ng T e s t” . ( 4 ) U s ers a re re q

u i red t o in s ta ll a W in d o w s s y s t e m , s in c e t he s o f t w a re c a n o nly run o n W i nd o w s s y s t em . 

### ( 1 ) I f t he f i rmw a re up gr a de is a v a i l a b l e, p l e a s e up gra de i t by refe r ring t o t he F i r m w a re U p g r a de in t he Ap p e n di x . 

### ( 2 ) T h i s s tep is re q

u i red t o u s e t o g e t

her w i t h t he a ss i s ta nt s o f

t w a re t o o b ta in m o r e de ta i l s . 

### C o n f i gur a t i o n In f

o rm a t i o n A i rcr a f t C on f igur ati on In f

o rm ati on M o t o r E S C P r op el l er B att e ry W ei g ht S 9 0 0 D J I - 4 2 1 6 D JI - 4 0 A Z - B L A D E - 1 7 × 6 . 0 In c h 6S - 1 2 0 0 0 6 8 00 g F4 5 0 D J I - 2 3 1 2 D JI - 20A Z - BL A D E - 9. 4 × 5 . 0 In c h 4 S - 5 00 0 8 9 0 g F 55 0 D J I - 2 3 1 2 D JI - 20 A Z - BL A D E - 9. 4 × 5 . 0 In c h 4 S - 5 00 0 1 53 0 g 

### R e c o mm en d e d 

### P ar a mete r s A i rcr a f t B a sic G a in Attitu d e G a in M ax An g ula r Rate P it c h R o l l Ya w V e rti c al P it c h R o l l P it c h R o l l S 9 0 0 1 0 0 1 0 0 1 0 0 1 0 0 1 6 0 1 6 0 22 0 220 F4 5 0 95 95 70 1 0 0 1 0 0 1 0 0 3 0 0 3 0 0 F 55 0 11 0 1 0 0 8 0 1 0 0 1 0 0 1 0 0 3 0 0 3 0 0© 20 1 5 D JI . A l l Rights Re se rv e d . 

### 10 | 

# B a s ic F ly i n g C o n tr o l M o d e K

n o wl e dg e Ple a s e re a d t

he C o nt r o l M o de K

n o w le d g e c le a r ly b e f

o re u s a g e, t o k

n o w h o w t o c o nt

r o l t he a i r c r a f t . Di ff erent c o n t

r o l m o des w ill g i v e yo u di ff erent f ligh t pe r f o rm a n c e s . Ple a s e ma ke s ure yo u under s t and t he f e a t u res a nd di ff eren c es o f t

he t hree c o nt

r o l m o de s . G P S A TT I . M o de ( W i th GPS M o du l e ) A T T I . M o de M a nu a l M o de R u d der An g ul a r V el o c i t y C o m m a nd L i ne a ri ty M a x i mum ru d der a ngul a r v el o c i t y is 1 50 ° / s Y E S C o m m and S ti c k Me a n i ng Mul t i a tti t ude c o n t r o l; S ti c k c e n t e r p o s i ti o n f o r 0  ̊ a tti t ud e , i t s end

p o i nt is 35  ̊ . M ax - a ngul a r v el o c i ty is 1 50 ° / s . No a tti t ude a ngle l i mi ta ti o n a nd v er ti c a l v el o c i t y l o c kin g . A l ti t ude Loc k M a i nt a in t he a l ti t ude be s t ab o ve 1 m e t e r f r o m gr o und. NO L o c k p o s i ti o n if GPS s i g n a l S ti c k R ele a s ed is a de qu a t e.

When GPS s i g n a l h a s been Only a tti t ude s ta bili z i n g . NOT R e c o mm e n d Only pe r f o rm i ng a tti t

ude G P S L o s t l o s t f

o r 3 s , s y s t em ent ers ATT I . M o de a uto m a ti c a ll y . s ta bili z i ng w i t h o ut p o s i ti o n l o c k . --- A tti t ude & s pe e d mi x t

ure c o nt r o l en s ures s t abili t y S a f e ty Enh a n c ed F a i l - S a f e(P o s i ti o n l o c k when h o v er i ng ) Aut o Le v el F a i l - S a f e (A tti t ude s ta bili z i ng ) De p ends o n e x pe r i en c e. W i t h GP S / C o m p a s s m o dule and t he f a i l s a f e re qu i re m ent s a re s a ti s f i ed, in e ac h C o nt

r o l M o de ( i n c lud i ng G P S M o de, A TT I . M o de, M a n u a l M o de and I OC M o de), t h e a i r c r a f t w i ll enter t he f a i l s a f e M o de. A p p l i c a ti o ns AP w o rk Sp o rt s f l yin g . --- 

## S tart & S t op M o t or K

n o wl e dg e (1) Bo t

h I mm edi a t ely M o de and I ntell i g e n t M o de a re a v a i l a b l e in t he A ss i s ta nt S o f

t w a re: A dva n c ed - >M o t o r - > S t o p T y pe. ( 2 ) St o p M o t o r m e t

h o d is def

aul t ed t o Im m edi a tely M o de . Ple a s e g et t o k

n o w w ell ab o ut t

h i s s e c ti o n bef

o re f l yi ng . **1** S t a rt M o t o r : Pu s h i ng t hr o ttle s ti c k bef

o re t a ke o f

f w ill n o t s t a rt the m o to r s . Y o u h a v e t o e x e cut e any o ne o f f o ll o w i ng f o ur C o m bin a ti o n S ti c k C om m an ds ( C SC ) t o s t art t he m o t o r s :© 20 1 5 D JI . A l l Rights Re se rv e d . 

### 11 | **2** S t o p M o to r : W e p ro v i de t w o o p ti o ns t o s t o p m o t o rs in t he a ss i s ta nt s o f

tw a r e : I mm e di a tely a nd In tell i g e n t . (1) I m m edi a te l y M o de: I f yo u s ele c t t h i s mo de, in a ny c o nt

r o l m o de, o n c e m o t o rs s ta rt a nd t hr o ttle s ti c k i s o v er 1 0 % , m o t o rs w ill n o t s t o p i mm edi a te l y o nly when t hr o ttle s ti c k is b a c k u nder 1 0% t he m o t o rs w i ll s t o p. I n t h i s c a s e, if yo u pu s h t

he t hr o ttle s ti c k o v er 1 0% w i t h i n 5 s e c o nds a f

t er m o t o rs s t o p, m o to rs w ill re - s ta rt , C S C is n o t neede d . I f yo u d o n ’ t pu s h t hr o tt le s ti c k a f

t er m o t o r s s ta rt in t

hree s e c o nd s , m o t o rs w ill s t o p a uto m a ti c a ll y . ( 2 ) I n tell i g ent M o de: B y u s i ng t h i s m o de, di ff

erent c o nt

r o l m o de h a s di ff

erent w a y o f s t o p p i ng m o t o r s . I n M a nu a l M o de, o nly e x e cutin g CS C c an s t o p m o t o r s . I n A TTI . M o de o r GPS ATT I . M o de, a ny o ne o f f o ll o w i ng f o ur c a s es w ill s t o p m o to r s : a ) Y o u d o n ’ t pu s h t

hr o ttle s ti c k a f

t er m o t o rs s t art w i thi n t

h ree s e c o nd s ; b) E x e cuti ng C S C ; c ) T hr o ttle s ti c k un der 1 0 % , a nd a f ter l a nding f

o r m o re t h an 3 s e c o nd s . d) I f t he angle o f m

ul ti - r o to r is o v er 70 ° , a nd t hr o t t le s ti c k under 1 0 % . 

## N o te s o f I n t e ll i g e nt M o d e

(1) I n AT T I . / G P S A T TI . M o de, i t h a s l anding j ud gm e n t , wh i c h w ill s t o p m o t o r s . ( 2 ) Sta rt m o t o rs in ATTI . / GPS A TT I . M o de, yo u h a ve t o e x e cut e C S C and t hen pu s h t

hr o ttle s ti c k o v er 1 0% in 3 s e c o nd s , o t herw i s e m o t o rs w ill s t o p a f t er 3 s e c o nd s . (3) Dur i ng n o rm a l f

ligh t , o nly pull t

h r o ttle s ti c k un der 1 0% w ill n o t s t o p m o to rs in a ny c o nt r o l m o d e . ( 4 ) F o r s a f

e t y re a s o n, w

hen t he s l o pe angle o f m

ul ti - r o t o r is o v er 70° dur i ng t he f light in ATTI . / GPS AT T I . M o de ( ma y be c au s ed b y c o ll i s i o n, m o t o r and E S C er r o r o r p ro p e ll er b r o ken d o w n), a nd t hr o ttle s ti c k is under 1 0 % , m o t o rs w ill s t o p a uto m a ti c a ll y . 

## N o te s o f I n t e ll i g e nt M o d e & I mm e d i at e ly M o d e

(1) I f yo u c h oo s e t

he I m medi a t ely M o de , yo u s h o ul d n o t pull t hr o t tle s ti c k un d er 1 0% dur i ng f ligh t , be c au s e i t w i l l s t o p m o to r s . I f yo u do i t a cc i de n ta ll y , yo u s h o ul d pu s h t he t h ro ttle s ti c k o v er 1 0% in 5s t o r e - s t a rt m o to r s . ( 2 ) DO NOT e x e cut e the C S C dur i ng n o r m a l f light w i th o ut a ny re a s o n, o r i t w ill s t o p m o t o rs a t o n c e. (1) I f yo u c h oo s e t

he I ntell i g ent m o de, a nd t he t hr o ttle s ti c k is under 1 0 % , t h i s w ill t rig g er t he l a nding P r o c edur e , in a ny c o nt r o l m o d e . I n t

h i s j ud g m ent , pi tc h, r o ll a nd ya w co nt r o ls a re denied e x c ept t h e t hr o t tle, b u t m

u l ti - r o t o r w ill s ti ll aut o le v e l . ( 2 ) I n a ny c o nt

r o l m o de, DO NOT pull t hr o t t le s ti c k under 1 0% dur i ng n o rm a l f light w i t h o ut a ny re a s o n. (1) Any o f t

he s e t w o cu t o f f t y pes w ill o nly w o r k p r o per ly if T X c a li b r a ti o n is c o rr e c t d o ne. ( 2 ) I n f

a i led - s a f e, C S C is denied by t

he m a in c o nt

r o ll e r , m o t o rs w ill h o ld t

he i r s ta t e .© 20 1 5 D JI . A l l Rights Re se rv e d . 

### 12 | 

## S t e p 

# 1 C o mp a ss C a l ib r a t i on W i th o ut GPS m o dule, p l e a s e s kip t h i s s te p . I f yo u u s e w i t

h G P S m o dul e , f

o ll o w s t e p - b y - s t ep f

o r c a libr a ti o n. (1) DO NOT c a l ib r a t e yo ur c o m p as s w here t here is m a g ne t i c i nt erfer e n c e , s u c h a s m a g ne t i te, c a r p a rk , a nd s t eel rein f

o r c e m e n t under the g r o und. ( 2 ) DO NOT c a rr y f

er r o m a g n e ti c m a t eri a ls w i t h yo u dur i ng c a libr a ti o n, s u ch a s ke y s o r c ell ph o ne s . (3) C o m

p as s m o dule C A

N NOT w o rk in t he p o l a r c i r c l e. ( 4 ) C o m

p as s C a libr a ti o n is v ery i mp o rta nt , o t herw i s e t h e s y s t e m w ill w o rk abn o rm a l. 

### C a l ib r a ti o n Pr o c e d

u r e s 1 . S w i t c h o n t

he t r a n s mi t t er, a nd t hen p o w e r o n aut o pil o t s y s te m ! 2 . Qu i ckl y s w i t c h t

he c o nt r o l m o de s w i t c h f

r o m GP S M o de t o M a nu a l M o de a nd b a c k t o GP S M o de ( o r f r o m G PS M o de t o AT T I . M o de and b a c k t o G P S M o d e ) f o r m o re t h an 5 ti m e s , T he LED i nd i c a to r w i ll t urn o n c o n s ta ntl y y ell o w s o t h at t he a i rc r a f t i s re a dy f

o r t he c a libr a ti o n . 3. ( F i g . 1 ) H o ld yo ur Mul ti - r o t o r h o ri z o nt a l a nd r o t at e i t ar o und t he g r a v i ta ti o n a l f o r c e line ( ab o ut 3 6 0 o ) un ti l t he L ED c h a nges t o c o n s t ant gr e en, and t hen g o t o t

he ne x t s t ep. 4 . ( F i g . 2 ) H o ld yo ur Mu l ti - r o t o r v e r ti c a ll y a nd r o t at e i t ( i t s n o s e is d o w nwa rd ) ar ound t

he gr a v i ta ti o n a l f

o r c e line ( ab o ut 3 6 0 o ) unti l t

he L ED t urn s o ff , m e a n i ng t

he c a libr a ti o n is f

in i s he d .

F i g . 1 F i g . 2 5. I f t he c a libr a ti o n w a s s u cc e ssf ul, c a libr a ti o n m o de w ill e x i t a uto m a ti c a ll y . I f t he L ED keeps f

l a s h i ng qu i c k

l y R ed, t he c a libr a ti o n h a s f

a i le d . S w i t c h t

he c o nt r o l m o de s w i t c h o ne ti m e t o c a n c el t h e c a libr a ti o n, a nd t hen re - s t a rt f

r o m s t ep 2 . (1) When t

he GPS is abn o rm a l, t

he M a in c o nt

r o ll er w ill t ell yo u by t

he L ED b l in ki ng R ed and Ye ll o w a l t ern a tely ( ), di sab l e t he G PS M o dule, and a u to m a ti c a ll y e n t er t he a i r c r a f

t in t o t he ATT I . M o de. ( 2 ) Y o u d o n ’ t need t o r o ta t e yo ur m u l ti - r o t o r o n a p r e c i s e h o ri z o nt a l o r v ert i c a l s ur f a c e, b u t ke e p a t le a s t 4 5° di ff

eren c e b e t

w een h o ri z o nt a l and v e r ti c a l c a libr a ti o n. (3) I f yo u keep h a v i ng c a libr a ti o n f a i lur e, i t mi g ht s ug g e s t t h at t h e re is v ery s t

r o ng ma g ne t i c i nt erfere n c e a r o und t

he G P S / C o mp a s s m o dule, p l e a s e a v o i d f l ying in t h i s a r e a . ( 4 ) When t o do r e - c a libr a ti o n a ) T he f

light f i eld is c h a ng e d . b) When t

he m u l ti - r o t o r m e c h a n i c a l s e t

up h a s c h a ng e d:  I f t he GP S / C o m

p a s s m o dule is r e - p o s i ti o ned.  I f ele ct

r o n i c de v i c es a re a d d ed / re mo v ed/ r e - p o s i ti o ned ( M a in C o nt r o ll e r , s er v o s , b a tterie s , e tc . ) .  When t

he m e c h a n i c a l s t

r u ct u r e o f t he m ul ti - r o t o r is c h a nged.© 20 1 5 D JI . A l l Rights Re se rv e d . 

### 13 | c ) I f t he f light dir e c ti o n ap p e a rs t o be s h if ti ng ( m e an i ng t

he m u l ti - r o to r d o e s n ’ t “fly s t r a i g ht”). d) The LED indi c a to r o f t en indi c a tes abn o rma li t y b l inkin g when t

he m ul ti - r o t o r s pin s . ( I t i s n o rm a l f o r t h i s t o h ap p en o nly o cc a s i o n a ll y) 

## S te p 

# 2 A ss e mb ly Ch e c kin g L i s t P l e a s e c h e c k e a ch 

### item, to m ak e s ur e f o r 

### s a f et y . A ny o f t he f o ll o w i ng mi s ta k es w ill le a d to a d anger o us a cc i d e nt , d o ub l e ch e c k a ll t he s e i te m s : (1) R o ta ti o n dire c ti o n o f m o t o r is o p p o s i t e ( 2 ) I n f irm c o nn e c ti o n b e t

ween t he m o t o r a nd t

he E S C (3) Wr o ng o r in f

irm in s ta ll a ti o n o f M a in c o nt r o ll er ( 4 ) Wr o ng o r in f

irm c o nne c ti o n b e t

w een the m a in c o nt r o ll er a nd E S C . (5) P r o pe l ler in s ta ll a ti o n m i s ta k e ( 6 ) M a g ne t i z a ti o n o f the c o m p a s s M a ke s ure t

he f o ll o w i ng i t e m s a re c o rr e c t . (1) M a ke s ure yo u h a ve a ss e m b l ed yo ur m

u l ti - r o t o r c o rr e c t l y. ( 2 ) M a ke s ure yo u h a ve d o ne t he c o n f i g ur a ti o n p r o c e dur e c o rr e c tl y . (3) M a k e s ure a ll c o nne c ti o ns a re in g oo d c o ndi t i o n. ( 4 ) M a ke s ure b atteries a re f ully c h a r g ed f

o r yo ur t r a n s mi tt e r , aut o pil o t s y s te m and a ll de v i c e s . 

## S te p 

# 3 B e f

o r e F l i ght C a rr y o ut the 

### f

o ll ow ing p r o c e d

ur es (i s b as ed o n 

### Int e l l i g ent Mo d e o f Mo t o r S t o p ) to m ak e s ur e 

### a l l c o n f i gu r a t i o ns a r e c o rr e c t. R e f er to t he 

### Ap p e n dix - > L E D D e s c ri p t i o n f o r m o r e 

### L E D d et a i l s . 1 . A l w ay s s w i t c h o n t he t r a n s mi tt e r f

i r s t , t hen p o we r o n m

ul ti - r o t o r! 2 . K eep t

he a i r c r a f

t s ta ti o n a ry un ti l t

he s y s t e m s t a rt and s el f - c he c k h a s f

in i s hed ( ) . A f t er t h a t , t he LED m a y b l ink Yell o w 4 ti m es qu i ckl y ( ). St a rt m o t o r is di sab le dur i ng LED b l i nkin g Yell o w 4 ti m es qu i ck l y ( ), a s t he s y s t em is w a rm i ng up . 3. A f t er t he 4 ti m es Yell o w L ED di s ap p e a r s , t o gg le t he c o n t r o l m o de s w i t c h o n yo ur t r a n s m i t ter t o m a ke s ure i t is w o rki ng p ro pe rl y . F o r e xamp le, LED b l in k s ( ), wh i ch m e ans t he s y s t em is i n AT T I . M o de a nd t he GPS s i g n a l is w o r s t Ch e c k i t w i t h L E D indi c a to r t o s p e c i f y t he curre n t w o rki n g m o de f o r M C . S ee f

o ll o w i ng t ab l e f o r de ta i ls ab o ut L ED indi c a to r; (1) There a re M a nu a l M o de and ATTI . M o de w i t h o ut a GP S / C o m

p a s s m o dule, n o GPS s i g n a l s t a t us LED indi c a to r. ( 2 ) A f t er c o nn e c t i ng t o t

he GP S / C o mp a s s m o dule, GPS A T TI . M o de is a v a i l a b l e , a nd GPS s i g n a l s ta t us L ED indi c a to r is a v a i l a b l e .© 20 1 5 D JI . A l l Rights Re se rv e d . 

### 14 | C o nt r o l M o de LED I nd i c a to r GPS S i g n a l St a t us L ED I ndi c a to r M a nu a l M o de: NO LED ATT I . M o de: ( indi c a tes t h at is s ti c k ( s ) n o t at c ent er) GPS M o de : ( indi c a tes t h at is s ti c k ( s ) n o t at c en te r ) S i g n a l is be s t (GPS s a tell i tes > 6 ) : NO LED S i g n a l is w ell (GPS s a tell i t es = 6 ) : S i g n a l is b ad (GPS s a tell i t es = 5 ) : S i g n a l is w o r s t (GPS s a tell i t e s < 5 ) : 4 . K eep t

he a i r c r a f

t s ta ti o n a ry , a nd t

hen pu s h b o t

h s ti c k s t o t

he left b o t t o m o r right b o tt o m ( s h o wn a s t he f o ll o w i ng c h a rt , def

i n e d a s C o m

b i n a ti o n S ti c k C om m a nds ( C SC ) ) , t o s t a rt t he m o t o r s .

5. R ele a s e t

he y aw , r o ll a nd pi tch s ti c k s a nd keep t hem a t t h e mi d p o i nt , a nd the t

hr o ttl e s ti c k und e r t

he mi d p o i nt . T hen c he c k w

h e t her a ll p r o pe l lers a re r o ta ti ng c o rr e c tl y . 6 . St o p m o to r s , p o w e r o f f t he Mul ti - r o t o r . 7. M a ke s ure a ll s e tti ng s a nd c o n f i g ur a ti o ns a re c o r

r e c t and t

hen yo u c an t a ke o f

f yo u a i r c r a f

t . 

### Af ter p ow er 

### o n , if a bn o rm a l LED I n di c a to r o c c ur s , p l e a s e refer t o t he Abn o r m a l LED in s tr

u c ti o n in t

he FA Q a nd a i ds t r o ubl e s h o o tin g . 

## S t e p 

# 4 F lyin g T e s t 1 . C h oo s e an o pen s p a c e w i t h o ut o b s t

ru c ti o n, t a ll buildings and c r o wds a s f l ying f i le d . Pl a c e t

he a i r c r a f

t 3 m e t ers a wa y f

r o m yo u a nd o t

her s , t o a v o i d a cc i dent a l in j u r y . 2 . I f in GPS AT T I . M o de, p l a c e t he a i r c r a f

t in a n o pen s p a c e w i th o ut bui l dings o r t ree s . T a ke o f

f t he a i r c r a f

t a f t er 6 o r m o re GPS s a tell i t es a re f o und ( Red LED b l in k s o n c e o r no b link in g ). I f in M a nu a l M o de o r A T T I . M o de, yo u c an s kip t

h i s s tep. 3. S ta rt - up (1) S w i t c h o n t

he t r a n s mi tt er f

i r s t , t hen p o w er o n m

ul ti - r o to r! K eep t

he a i r c r a f

t s ta ti o n a ry unti l t

he s y s t em s t ar t a nd s el f

- c he c k h a s f

in i s hed. ( 2 ) Ple a s e w a i t f

o r t he s y s t em t o w arm up g ra du a ll y w i t h t h e LED b l i n ks Yell o w 4 ti m es qu i c k l y ( ). Y o u s h o uld n o t s ta rt t he m o to rs unti l t

he b l i n ki ng di s ap p e a r s . (3) K eep t

he a i r c r a f t s ta ti o n a ry , a nd e x e cut e t he C S C t o s ta rt t

he m o t o r s . ( 4 ) R ele a s e t

he y a w , r o ll a nd pi tch s ti c k s a nd keep t hem at t he mi d p o i nt , a t t

he s a m e ti m e r a i s e t

he t hr o ttl e s ti c k f

r o m t he b o tto m . T he m o t o rs w ill s t o p if yo u do n o t pu s h t he t hr o ttle s ti c k f

r o m t he b o tt o m w i t

h i n 3 s ec a nd yo u w ill need to r e - s t a rt t he m o to r s . (5) K eep r a i s i ng t

he t hr o t tle s ti c k un ti l a ll t he r o t o rs are w o rkin g , p us h t he t hr o tt le s ti c k t o t

he mi d p o in t a nd t hen t a ke - o f

f yo ur m

u l ti - r o t o r g en tl y , p ay a t t ent i o n n o t t o pu s h t he s ti c k e x c e s s i v el y .© 20 1 5 D JI . A l l Rights Re se rv e d . 

### 15 | ( 6 ) P a y a tt en t i o n t o t he a i r c r a f

t m o v e m e n t at a ny ti m e when f l ying, a nd u s e t

he s ti c k s t o a dju s t t

he a i r c r a f t ’ s p o s i ti o n. K eep t

h e y aw , r o l l , pi t ch and t

hr o tt le s ti c k s a t t

he mi d p o i n t t o h o v er t

he a i r c r a f

t a t t he de s i red he i g h t . 

### 4 . Lo w er t

he a i r c r a f t s l o w l y . Pull t he t

hr o ttle s ti c k t o t

he b o tt o m and t

hen e x e cu te t

he C S C t o s t o p t

he m o to rs a f t er l a nding. 

### 5 . Ple a s e a lw a y s p o w er o f f t he Mu l ti - r o to r f

i r s t , a nd t hen s w i t c h o f

f t he t r a n s mi tt er a f

t er l a nding. 

### FL Y IN G N O TE S (VERY IM P O R T A N T ) ! ! ! (1) I f t he wa rm up w a i tin g is l o nger t h an 2 mi nu t es ( the 4 ti m es Yell o w b l in k c o n t i nu e s ), p l e a s e p o w er o f f f o r 1 0 mi nu t e s , c o ld s ta r t , a nd t hen c o nne c t t

h e a ss i s ta nt s o f

t w a re, en ter t

he " T oo l s " - > I MU c a libr a ti o n, c a rr y o ut t

he Ad v an c e d c a libr a ti o n. ( 2 ) I f yo u en ab l e t

he Imm edi a te l y M o de o f M o t o r S t o p ; yo u s h o uld n o t pull t hr ottle s ti c k under 1 0% dur i ng f ligh t , be c au s e i t w ill s t o p m o t o r s . I f yo u do i t a cc i d ent a ll y , yo u s h o uld pu s h t he t h r o tt le s ti c k o v er 1 0% in 5s t o r e - s t a rt m o t o r s . (3) DO NOT e x e cu t e t he C S C dur i n g n o rm a l f

light w i th o ut a ny re a s o n, o r i t w ill s t o p m o t o rs at o n c e. ( 4 ) P a y a tten ti o n t o t he GPS s a tell i t e s t a t

us LED indi c a to r. Ba d GPS s i g n a l m a y le a d t he a i r c r a f

t to dr i f t when h o v eri n g . (5) DO NOT f

ly ne ar t o f

er r o m a g ne t i c s u

b s ta n c e s , t o a v o i d s t

r o ng m a g ne ti c i nt erfere n c e w i t h t he GP S . ( 6 ) Ple a s e a v o i d u s i ng GPS AT T I . M o de in t he a re a s , where G P S s i g n a l is m o s t li k e ly b a d . (7) I f t he L ED f l a s hes qu i c kly R ed t

h en t h i s indi c a t es b att er y v o l t a g e is l o w , l a nd A S A P . ( 8 ) I f t

he t r a n s mi t t er indic a tes l o w - b att e r y a l a rm , p l e a s e l a nd A S A P . I n t h i s c o n d i ti o n t

he t r a n s m i t t er m a y c au s e t

he a i r c r a f t t o g o o ut o f c o nt

r o l o r e v en c r a s h. ( 9 ) I n GPS AT T I . M o de, m a ke s ure t h at t he h o m e p o i nt is re c o rd ed when t he GPS s i g n a l is w ell ; o t herw i s e t he h o m e p o in t re c or ding ma y be n o t s o p r e c i s e. (1) In ATT I M o de, t

hr o t tle s ti c k c ent e r p o s i ti o n is f o r 0 m / s a l o ng t

he v er ti c a l dire c ti o n. Y o u s h o uld keep t he p o s i ti o n o f t

hr o ttle s ti c k h i gher t

h an 1 0% f

r o m c ut - thr o ttl e dur i n g t he f li g ht ! I n an y c o nt r o l m o de, D O NOT pu l l t hr o t tle s ti c k under 1 0% dur i ng n o r m a l f light w i t h o ut any re a s o n. ( 2 ) I t is re c om m end e d t o l and t he a i r c r a f t s l o w l y , t o p r e ve n t t

he a i r c r a f t f r o m d ama g e w

hen l a nding. (3) I f Lo w - Vo l t a g e A l a rm is s e t , t h e a i r c r a f

t w i ll a c t a cc o rd in g t o t he c o n f i g ur a t i o n o f t

he A ss i s ta nt S o f t w a re o n c e Lo w - Vo l t a g e A l ar m is t rig g ere d. M a ke s ure yo u rem e m ber w h at yo u h av e s et bef o re. ( 4 ) I f F a i l - S a f

e f un c ti o n is s e t , t

he a i r c r a f

t w ill a c t a c c o rd i ng t o t he c o n f i g ur a t i o n o f t

he A ss i s ta nt S o f t w a re o n c e F a i l - S a f

e is t rig g ere d . M a ke s ure yo u re m e m ber w h a t yo u h av e s et bef o re.© 20 1 5 D JI . A l l Rights Re se rv e d . 

### 16 | **me Po**  **i nt**  **Stay hov** 

**to Go**  **- Hom**  **ocation >**  **20m f**  **i rst**  **cation ≤**  **20m H** 

What tr i gge r ed f a il s a f e T h e aircraft b e h a v i o r after f a il s a f e How to r eg a i n c o ntr o l P r e c aut i o n s 

# Adv a nced F u nc ti o ns A 

# 1 F a i l S a fe An 

### intr o d u c ti o n o f G o - H o m e a

n d 

### L an d i

### n g .

**Record Home**  **Point er**  **Ho** 

## 1 **Multi -**  **rotor T**  **x Ground**  

## 2 **Signal l**  **ost T**  **x** 

## 3 **Ready e**  **Go -**  **Home Current**  **l Signal**  **lost >3s**  20 m **Go -**  **Home Ascend**  **over 15s,**  **then l**  **and Tx**  **T x**  

## 4 **5 Current**  **lo T**  **x** 

## 6 H o m e - p o i n t : B e f

o re ta ke o ff

, current p o s i ti o n o f m

ul ti - r o t o r w ill be s a v ed a s h om e - p o i nt by M C auto m a ti c a ll y w hen yo u s t art t

he m o t o rs f

o r t he f i r s t ti m e a f

t er 6 o r m o re GPS s a tell i t es a re f o und (red light b l in ks o n c e o r no b l inki ng ) f o r 1 0 s e c o nd s .

(1) Ple a s e m a ke s ure t o re c o rd t h e h o m e - p o i nt bef

o re ta k e o ff

, a nd c le a r ly k

n o w w here i t i s . ( 2 ) Duri ng g o - h o m e t

he n o s e dire c ti o n o f t

he a i r c r a f t is f a c i ng t o w a rd t

he h o m e - p o i nt , t

he a i r c r a f t i s f l ying dire c tly f

r o m t he c urrent p o s i ti o n t o t

he h o m e - p o i nt . (3) Y o u c a n re g a in t

he c o nt r o l dur i ng t

he a i r c r a f t is h o v ering 1 5 s e c o nd s . The f l o w c h a r t of failsafe and how to r eg a i n c o n tr o l This s e c ti o n will demonstrate the w o rk i n g l o g i c of failsafe and how to r eg a i n c o ntr o l. Th e following de s c rip ti o n is e ff e c ti v e only wh e n : 1. Th e a i r c r a f

t is in f li g ht . 2. Th e GPS works n o rm a ll y and s i g n a l is good ( ≥ 6 s at e lli t e , the LED blinks a s i n g l e red li g ht or no red li g ht) . (1) The a i r c r a f

t flies far a w ay , TX is on but t h e s i g n a l is w e a k . A tt i t u de M o de : (1) the a i r c r a f t will level i t s a tt i t u de i mm ed i a t e l y (2) 3 seconds l a t e r , failsafe is tr i gge r ed an d a i r c r a f t will start to go h o m e . (3) If s i g n a l is r eg a i n ed d ur i n g (1) or (2), i t will resume n o r m a l f li g h t i mm ed i a t e l y . GPS M o de : (1) the a i r c r a f t will slow down and h o v e r . (2) i f the s i g n a l is restored within 3 seconds (TX and r e c e i v e r c o nn e c t ed ) , the system will i mm ed i a t e l y return to n o r m a l o pe r a t i o n ; does not enter failsafe. (3) if not r e c o nn e c t ed within 3 s e c , the system will enter failsafe, then even if t h e s i g n a l is r e s t o r ed , the system will not exit f a il s a f e . A tt i t u de M o de : In A tt i t u de Mode a s

soon as you get s i g n a l you c a n r eg a i n c o n tr o l . GPS M o de : s w i t c h the TX m o de s w i t c h to AT TI , if the r e c e i v e r i s c o nn e c t ed , then you will r eg a i n c o n t r o l . (2)Turn off t h e TX (we a ss u m e you want t o tr i gge r f a il s a f e ) In t h i s c a s e , the be h av i o r of the a i r c r a f t is the same as i n the above c o n d i t i o n . If you want the a i r c r a f t to R e t ur n H o m e , p l e a s e do not t ur n the TX back on within 3 s e c o n d s * , o t h e r w i s e the a i r c r a f t will exit failsafe mode i mm ed i a t e l y . If you choose to turn off the TX, you must be pretty sure that y o u know how to r eg a i n c o n t r o l . H e r e we offer a m e t h o d , p l e a s e r e a d c ar e f u ll y . We s t r o n g l y recommend you DO NOT try t h i s , because there are t h r ee types of r i s k : (1) Y o u must be pretty c l e ar whether the H o m e - p o i n t is OK for l an d i n g o r n o t . ( Y o u have to understand the de f i n i t i o n of H o m e - p o i n t well and t h e w o r k i n g process of f

a il s a f e ) (2) If there are tall b u il d i n g s ar o un d , the a i r c r a f t may be obstructed on t h e w ay . (3) When GPS s i g n a l is bad or GPS is not working, failsafe will not w o r k . When you turn off the TX, use the f o ll o w i n g method to r eg a i n c o n tr o l : (1) Switch the TX s w i t c h to G P S . (2) and then put t h r o tt l e to the c e n t e r p o s i t i o n ( g r e a t e r than 3sec after s w i t c h i n g o ff , i m p o rt a n t ) , you can now turn the TX back o n . (3) then you can s w i t c h the TX C o nt r o l m o de s w i t c h to AT TI to r eg a i n c o n t r o l . N o t e : if you start the m o t o r s , but do not push the t h r o tt l e to take - off the aircraft, in t h i s case i t is very dangerous to t ur n off the TX, because the a i r c r a f t will take off a u t o m a t i c a ll y , so do not try t h i s . * If s i gn a l l o s t for more than 3 seconds failsafe will be tr i gge r ed , if s i gn a l r eg a i n ed within 3 seconds it will exit failsafe i mm edi at e l y .© 20 1 5 D JI . A l l Rights Re se rv e d . 

### 17 | 

## A 

# 2 L o w - V o l ta g e A l e rt I n o r d er t o p r e v ent yo ur m ul ti - r o t o r f

r o m a c r a s h o r o t

her h a rm f

ul c o n s equen c es c au s ed by l o w b att ery v o l ta g e, t here a re t

w o le ve ls o f l o w v o l t a g e p ro te c ti o n a v a i l a b l e t o u s e. Y o u c an ch oo s e t o u s e o r n o t t o u s e t he m ; h o w e v er w e s t r o ngly r e c om m end u s i ng t he p ro te c ti o ns i f a v a i l a b l e! L o w - Vo l t a g e A lert is t o indi c a te t h at t he b a tt ery c a nn o t p ro v i de en o ugh p o w er f o r t he a i r c r a f

t , i n o r d er t o w a rn yo u t o l and t he a i r c r a f

t A S AP. Y o u c a n c o n f

i g ure th i s f un c ti o n in t

he a ss i s ta nt s o f

t w a re, and p l e a s e re a d t

he t e x t in t

he s o f t w a re c aref

ull y bef o re yo ur f

ligh t . M a ke s ure to c a rry o ut t

he Curren t Vo l t a g e C a libr a ti o n. T here a re b o t h f

i r s t l e v el a nd s e c o nd l e v el p ro te c ti o n s . T he f i r s t l e v el p ro t e c ti o n h a s L ED w a rni n g . D u ring s e c o nd le vel p ro t e c ti o n t

he a i r c r a f

t w ill l a nd auto m a ti c a ll y w i t h L ED w a rning. Me anw h i le t he c ente r p o i nt o f t

hr o ttle s ti c k w ill m o v e up s l o w ly t o 9 0% o f end p o i nt , yo u s h o uld l and A S AP t o p r e v ent yo u r a i r c r a f t f r o m c r a s h i ng ! I t is n o t f

o r f un, yo u s h o uld l a nd yo ur a i r c r a f t A S A P t o p r e ve n t yo ur a i rc r a f t f r o m c r a s h i n g o r o t

her h a rm f

u l c o n s equen c e s !! !

(1) C o n f

i g ure t he F a i l S a f

e f un c ti o n in t

he a ss i s ta nt s o f

t w a re - > “ A dva n c ed” - > “ F / S ” a nd re a d t he in s t ru c ti o n t h o r o ugh ly a nd c aref

ul l y . ( 2 ) C o n f

i g ure t he L o w - V o l ta g e A lert f

un c ti o n in t

he a ss i s ta nt s o f

t w a re - > “Adva n c ed” - > “V o l t a g e” a nd re a d t

he in s t ru c ti o n t h o r o ugh ly a nd c a ref

ul ly .© 20 1 5 D JI . A l l Rights Re se rv e d . 

### 18 | I OC S w i t c h I OC F un c ti o n O F F C o ur s e Lo c k H o m e Lo c k 

## A 

# 3 I nt e l li g e nt O ri e n t a t i o n C o n t r o l ( I O C) F l i ght (w i t

h GP S m o d

ul e ) Def i n i ti o n o f F o rw a rd Dire c ti o n: 

### M u l ti
- r o t o r w ill f

ly a l o ng t h i s dire c ti o n when yo u pu s h t he ele vat o r s ti c k ( ). 

## S t e p 

# 1 B e fo re Y o u 

## S t art U s u a ll y , t he f o rw a rd dire c ti o n o f a f

l ying m ul ti - r o to r is t

he s a me a s t

he n o s e dire c ti o n. B y u s i ng I O C , where v er t h e n o s e p o i nt s , t

he f o rw a rd dire c ti o n h a s n o t h i ng t o do w i t

h n o s e dir e c ti o n. T he r ed and b l ue a r r o w s o n t h e t r a n s mi tt e r a re c o r r e s p o nding t o pi t ch and r o ll o pe r a ti o ns in t he f o ll o w i ng di a g r a m .  I n c o ur s e l o c k f

l yi n g , t he f o rw a rd dir e c ti o n is t

he s a m e a s a re c o rd ed n o s e dire c ti o n. A ll t he f o ll o w i ng re qui rem ent s a re m e t : t

he aut o pil o t s y s t e m is in ATT I . M o de o r G PS A T TI . M o de.

N o rm a l f l ying C o ur s e L o c k F l yi ng  I n h o me l o c k f

l yi ng, t he f o rw a rd di r e c ti o n is t

he s a me a s t

he dire c ti o n f

r o m h o m e p o i nt t o m

u l ti - r o t o r. A l l t

he f o ll o w i ng re qui re me n t s a re m e t : 6 o r mo re GPS s a tell i t es a re f o und, in GPS A T TI . M o de, a nd t he a i r c r a f t i s f urt her t h an 1 0 m a w a y f

r o m t he h o m e p o in t .

N o rm a l f l ying H o m e L oc k F l yi ng 

## S t e p 

# 2 I OC S w i t c h S e tt in g B e f o re u s i ng t

he I OC f un c ti o n, yo u h a ve t o c h oo s e a 3 - p o s i ti o n s w i tc h o n yo ur t r a n s mi tt er a s t

he I OC s w i tc h , wh i ch is a l s o u s ed f

o r re c o rd i ng t

he o rient a ti o n, h o m e p o s i ti o n in c o rr e s p o nding m o d e s . R e f er t o t he a ss i s ta nt s o f

t w a re; c li c k t he “A dva n c ed” t o f

i nd t he “ I O C ” .

The ab o v e t ab l e is f

o r e x a mp l e . T he f

u n c ti o n o f t

he s w i tc h p o s i ti o n m a y be re v er s ed s in c e t he n o r m a l / re v er s ed s e t ti ng o f t

he s w i tc h c h a nne l . T o gg l e t he s w i tc h a n d o b s er

ve t he s li d er p o s i ti o n o f c h annel X 2 o n t

he a ss i s ta nt s o f

t w a re s creen, t

he c o rre s p o ndi n g a rea s h o uld t urn b l ue.© 20 1 5 D JI . A l l Rights Re se rv e d . 

### 19 | o v i ng dire 

## S t e p 

# 3 M e th o d o f Fo rw ard 

## D i re c t i o n a n d H o m e 

## P o i n t R e c or d i n g I f yo u u s e t

he I O C f un c ti o n, p l e a s e be a w a re o f t he F o rw a rd Dire c ti o n o f C o ur s e L o ck F l yin g , a nd t he h o m e p o i nt o f H o m e Loc k F l yin g . T here a re t w o w a y s t o re c o rd t

he f o rw a rd dire c ti o n and t

he h o m e p o i nt : M a nu a lly a nd Auto m a ti c a ll y . Y o u m a y c h oo s e any o ne re c o rd m e t h o d. The LED w ill b l in k Gr e en q u i ckl y if s u cc e ssf

ul l y re c o rd e d. C o ur s e L o c k H o m e L o c k

Auto m a ti c a ll y 30 s e c o nds a f t er yo u p o w er o n t

he aut o pil o t s y s t e m . B e f o re ta ke o ff

, t he curren t p o s i ti o n o f t

he a i r c r a f t w ill be s av ed a s h o m e p o i nt w hen yo u s t a rt t

he m o t o rs f o r t he f i r s t ti m e a f

t er 6 o r m o re G P S s a tell i tes h a v e been f

o und f o r 1 0 s e c o nd s . M a nu a ll y 30 s e c o nds a f t er yo u p o w er o n t

he aut o pil o t s y s t e m . T o gg le t h e I OC s w i tc h f r o m O f f t o C o ur s e L o ck , a nd b a c k t o O f f qu i ckl y 3 t o 5 ti m e s . A f t er 6 o r m o re GPS s a tell i tes h a v e been f o und. And t he a i r c r a f

t c a n be h o v erin g . T o gg le t h e I OC s w i tc h f r o m C o ur s e L oc k t o H o m e L o ck , a nd b a c k t o C o ur s e L o c k qu i ck l y 3 t o 5 ti m e s . DO N O T to gg l e t

h e s w i t c h b et

w e en O f f t o H o m e L o ck , s i n c e i t m a y c h ange t he re c o r ding o f t

h e F o r w a rd Dir e c ti o n o f C o ur s e L o c k . 

## S t e p 

# 4 I OC F 

## l y i n g T e s t T hen yo u c an do Co ur s e L oc k a nd H om e L oc k f l y ing t e s t . C a rry o ut an I OC f

light b y t

he f o ll o w i ng p ro c edur e . T he C o nt r o l M o d e LED w ill b l i nk Yell o w a nd Gr een a l t ern a ti v e l y ( ) t o indi c a te t he I O C m o de o nly when t he m a in c o nt

r o ll er is r e a ll y t o f

ly in C o ur s e L o ck , H o m e Lo c k m o de s . Dur i ng t he S T EP 1 : R e c o rd S T EP 2 : ON S T EP3: O F F S T E P 4 : ON a g a in s a m e f light C o ur s e Lo c k

S w i t c h S e ttin g R e c o rd t he F o rw a rd Dire c ti o n S et C o nt

r o l M o de s w i t c h a t GPS o r AT T I . p o s i ti o n, T o gg le I O C s w i tc h f

r o m O F F t o C o ur s e L o c k p o s i ti o n T o gg le I O C s w i tc h t o O F F p o s i ti o n T o gg le I O C s w i tc h

f r o m O F F t o C o ur s e L o c k p o s i ti o n

H o m e Lo c k

S w i t c h S e ttin g R e c o rd t he H o m e P o i nt S et C o nt r o l M o de s w i t c h a t GPS p o s i ti o n, T o gg le I O C s w i tc h f

r o m O F F t o H o m e L oc k p o s i ti o n T o gg le I O C s w i tc h t o O F F p o s i ti o n T o gg le I O C s w i tc h

f r o m O F F t o H o m e L o c k p o s i ti o n A i r c r a f t m c ti o n when pull p i tch s ti c k A i r c r a f t m o v i ng dir e c ti o n when pull r o ll s ti c k H o m e p o i nt A i r c r a f t ( t h e a rro w is p o i nt i ng t o t

he dir e c ti o n o f t

he a i r c r a f t n o s e )© 20 1 5 D JI . A l l Rights Re se rv e d . 

### 20 | I OC F LY IN G NO T E S !!!

(1) When Mul t i - r o to r is f l ying by h o m e l oc k f

a r a w a y f r o m yo u a nd t

he h om e p o i nt , p l e a s e DO N O T t o gg le t he I OC s w i tc h m any ti m es qu i ckl y s o a s t o a v o i d t he ch a nge o f h o m e p o i nt w i t h o ut y o ur a ttent i o n. (1) H o m e l o c k f

l ying re qui res t

h at 6 o r m o re GPS s a tell i tes a re f o und and t

he a i r c r a f t is f urt her t h a n 1 0m a w a y f

r o m t he h om e p o i nt . ( 2 ) I f t he I O C f l y ing r e qu i r e ment is n o t s a ti s f i ed, t h e aut o pil o t s y s t e m w ill q u i t I OC c o n t

r o l m o de. Ple as e be a wa re o f t

he L ED indi c a to r, t o k

n o w the curr e nt c o n t

r o l m o de o f t

he aut o pil o t s y s t e m . (1) B linking indi c a ti o ns o f I OC a re: a ) B e f o re m o t o rs s ta rt : b l ink , a ll s ti c k s (e x c ep t t hr o t tle s ti c k

) re t u rn to c e n ter; b l ink , s ti c k ( s ) (e x c ep t t

hr o ttle s ti c k) n o t a t c e nt e r . b) A f t er m o t o rs s t a rt and t

hr o tt le s ti c k is o v er 1 0% in 3 s e c o nd s : b l ink , a ll s ti c ks re t urn t o c ent er; bl i nk , s ti c k ( s ) n o t a t c e n ter. ( 2 ) B e f

o re yo u do t

he h o m e l o c k f

ligh t , yo u h a v e t o f

ly t he a i r c r a f

t o ut o f t he 1 0m r ange a r o und h o m e p o i nt , a nd t

hen f lip the I O C s w i t c h t o H o m e Lo c k p o s i ti o n t o f ly in h om e l o c k when a ll t he re qui rem ent s a re m e t . I f yo u h a v e a lr e a dy t o gg led t he I O C s w i t c h t o H o m e L o c k p o s i ti o n w hen t he a i r c r a f t is s ti ll in 1 0 m r a nge ar o und h o m e p o i nt , a nd t h i s is t h e f i r s t ti m e y o u a re g o i ng t o f ly in h o m e l o c k dur i ng t

he current f

ligh t , t hen if a ll t

he re q u i re m ent s are m e t , t he m a in c o nt r o ll er w ill c h a nge i nto h o m e l o c k a uto m a ti c a ll y when Mul ti - r o t o r f lies o ut t he 1 0m r a nge a r o und h o m e p o i nt . (3) When f

l ying in H o m e Lo c k m o d e , if a ny o f t he f o ll o w i ng s i t

u a ti o ns h ap p en, t

hen t he s y s t e m w i ll q u i t H o m e Lo c k f

l y ing a nd auto m a ti c a ll y e nt er C o ur s e Lo c k f l y i n g . T he a i r c r a f

t w ill f l y in C o ur s e L o c k u s i ng t

h e e a rl i er f

o rw a rd dire c ti o n. a ) The a i r c r a f

t f ly ’ s w i t hi n 1 0 m r ange o f t

he h o me p o i nt . b) Y o u t o gg le t

he c o nt r o l m o de s w i t c h t o t he A TT I . M o de. c ) The GPS s i g n a l b e c o m es b ad ( The G P S s i g n a l L ED is b l in ki ng R ed t w i c e o r t h r ee ti m e s ). ( 4 ) W e s ug g e s t t

h a t yo u s h o ul d kn o w c le a r l y wh i c h f ligh t l oc k m et

h o d yo u a re g o i ng t o f

l y , a nd yo u k n o w t he l o cked f

o rw a r d dire c ti o n o r h o m e p o i nt , bef o re yo u s w i t c h o n I O C m o de d uring the f ligh t .© 20 1 5 D JI . A l l Rights Re se rv e d . 

### 21 | 

## A

# 4 R e c e iv er A dv a

n c e d P r o t e c t i o n F u

n c ti o n Y o u a re a s ked t o en ab l e t h i s f un c ti o n by c o nn e c ti ng t o t he A ss i s ta nt S o f

t w a re, p l e a s e s et i t at t

he s e c ti o n o f B a s i c - > R/ C - > R e c e i v er Ad va n c e d P r o te c ti o n. I f yo u c h oo s e en ab l e i t , t

he F a i l S a f

e w ill be t rig g ere d if t

he f o ll o w i ng s i t

u a ti o ns o ccur dur i ng f

lig h t . A c c o rd i ng t o t

he di ff er e n c e o f t

he a i r c ra f t he i ght , t here are t

w o s i t u a ti o n s . 1 . Lo w er t

h an 1 0 0 m , t

he A /E /R c h a nnel is n o t at t he mi d p o i nt . 2 . H i g her t h an 1 0 0 m , t h e A/E /R c h a nnel is n o t at t he mi d p o i nt o r t

he t hr o t tle s ti c k is ab o v e t

he mi d p o in t . I n t he G P S M o de o r ATT I . M o de, i f t he re q u i re m en t a ) o r b) is s a ti s f i ed, a nd t he o ut put d ata o f f

o ur c h a nnels A/E /R /T h a v e n o t c h anged f o r 2 0 s e c o nd s , t

hen t he a i r c r a f t w ill h o v er a uto m a ti c a ll y . A f t e r t h a t , if t he o utput d a ta o f f o ur c h annels A/E /R/T s ti ll do n o t any c h anges and l a s t f o r 1 0 s e c o nd s , t

he aut o pil o t s y s t em w i l l t h i nk t h at t he d at a f r o m re c e i v e r is abn o rm a l, a nd t hen enter t

he F a i l S a f

e M o de. B rief i nt r o du c ti o n o f h o w t o q

u i t the F a i l S a f

e M o de I f t here is a ny c o mm a nd ch ange f r o m t he re c e i v e r , t

he aut o pi l o t s y s t em t

h i nks t h a t t he re c e i v er is re g a i ned. I n ATTI . M o de a nd M a nu a l M o de, i t w ill qu i t t he F a i l S a f

e M o de a uto m a ti c a ll y . I n G P S M o de, p l e a s e t o gg le t he c o n t r o l m o de s w i tc h t o t

he ATT I . M o de and M a nu a l M o de p o s i ti o n t o re g a in t he c o nt r o l. R e f er t o t he F a i l S a f

e s e c ti o n f

o r m o re de ta i l s .© 20 1 5 D JI . A l l Rights Re se rv e d . 

### 22 | 

## A 5 F l i gh t L i mi t s T he f light l i mi t s f

un c ti o n is def

ault en ab l ed in t

he N A Z A - M F li g ht c o nt r o l s y s t e m , i t ’ s a i m ed t o re s t ri ct t he f lyin g he i ght a nd di s t an c e o f t he a i r c r a f

t . T h e M ax H e i ght re s t

ri ct s t he v e rt i c a l di s t an c e bet w een t he a i r c r a f

t a nd t h e H o m e p o i nt , t

he M a x R a dius re s t

ri ct s t he h o ri z o nt a l di s ta n c e bet w een t he a i r c r a f t a nd t he H o m e p o i nt . T he def ault M ax H e i gh t is 2 0 0 0m a nd M ax R a dius is 2 0 0 0 m . U s ers c an wri t e t he v a lues o f t

he M ax H e i ght a nd M ax R a dius in t

he A ss i s ta nt s o f

t w a re, the r ange o f t

he M ax H e i gh t is 1 0 m - 1 0 0 0 0 0 m , t he r an g e o f t

he M ax R a dius is t

he s a m e. S o t

h a t t h e a i r c r a f t w ill f ly in t h e en t er e d r a nge, wh i ch is a c ylinder s p ac e ab o v e t he H o m e p o i nt .

(1) H e i gh t L i mi t w o rks when the c o nt r o l m o de is GPS o r AT T I . M o de . R a dius L i mi t w o rks wh en t he c o nt r o l m o de is GPS a nd t

h e s a tell i te nu m

ber ≥ 6 . ( 2 ) I f t he a i r c r a f t f lies o ut o f t

he li mi t s , i t ' s s ti ll c o nt

r o ll a b l e e x c ept f

l y ing f urt h e r a w a y . (3) I f t he c o nt r o l m o de is c h a nged t o GPS wh e n t he a i r c r a f t is o ut o f M a

x R a diu s , t

he a i r c r a f t w ill f l y b a c k w i t h i n t

he ent ered r a ng e . ( 4 ) The F a i l s a f

e a nd t he Gr o und S ta ti o n o pe r a ti o ns a re n o t re s t ri c t ed t o t

he F light L i mi t s .© 20 1 5 D JI . A l l Rights Re se rv e d . 

### 23 | 

# Ap pe n dix S p e c i f i c at i o n s G e n e ra l (1) Three M o des o f Aut o pil o t ( 4 ) S - B u s / S - B u s 2 R e c e i v er S u p p o rt B u i l t- I n F un c ti o ns ( 2 ) Enh an c ed F a il S a f e (5 ) PPM R e c e i v er S u p p o rt (3 ) L o w Vo l t a g e P r o te c ti o n ( 6 ) 2 - ax le Gi m b a l S upp o rt 

## P e rip h er a l S upp o rt ed Mul ti - r o t o r  Qu a d - r o t o r I 4 , X 4 ;  H e xa - r o t o r I 6 , X 6 , I Y 6 , Y 6 .  O ct o - r o t o r I 8 , V 8 , X 8 S upp o rt ed E S C o ut

p u t 4 0 0 H z refre s h f r e quen c y . R e c om m end e d T r a n s mi tt er P C M o r 2 . 4 G H z w i t h a min i m um 4 c h a nnel s . A ss i s ta n t S o f

t w a r e S y s t em R e q

u i r e ment W i nd o w s XP S P3; W i nd o w s 7; W i nd o w s 8 

## E l e c tri c a l & M e c h a

n i c a l W o rki ng V o l t a g e R ange  M C : 4 . 8 V ~ 5 . 5 V  PMU I nput : 7 . 4 V ~ 2 6 . 0 V (re c om m end 2 S ~ 6 S L i P o )

Out put ( V - S EN p o rt r e d w ir e ): 3 A @ 5V Out p u t ( V - S EN p o rt red w i r e )bur s t c urr e n t : 7 . 5A P o w e r C o n s u m p t

i o n  MAX : 1 . 5 W ( 0 . 3 A @ 5 V )  N o rm a l: 0 . 6 W ( 0 . 1 2 A @ 5 V) O p er a ti ng T e m

p er at ure - 1 0 ° C ~ 50 ° C ( 1 4 F ~ 1 22 F )  M C : 2 7g W e i gh t  GP S / C o m p a ss : 2 7g  PM U : 2 8 g  L ED: 1 3g  M C : 4 5 . 5 m

m × 3 2 . 5 m m × 1 8 . 5 mm D i m en s i o ns  GP S / C o m p a ss : 4 6 m m (di a me t er) x 1 0 m

m  PM U : 3 9 . 5 m m × 2 7 . 5 mm × 1 0 . 0 mm  L ED : 2 5 mm × 2 5 mm × 7 . 0 mm 

## F l i g ht P er f

o r m a n c e ( c a n be e ff

e ct ed by m e c h a n i c a l pe r f o rm a n c e and p a y l o a d s ) H o v ering A c curac y (G P S M o de)  V e rti c a l: ± ± 0 . 8 m  H o ri z o nt a l: ± ± 2 . 5m M ax Y aw Angul ar V el o c i t y 2 0 0 ° / s M ax T ilt Angle 3 5° M ax A s c en t / De s c ent Speed ± A s c e nt : 6 m / s , De s c en t : 4. 5 m

/ s© 20 1 5 D JI . A l l Rights Re se rv e d . 

### 24 | 

## M C /P M U F irmw ar e Up g ra d e Ple a s e f o ll o w t he p r o c edure f

o r s o f t w a re and f

irmw a re up gra de; o t

herw i s e t he s y s t em mi g h t n o t w o rk p ro pe rl y . F o r S AF E T Y RE A S ON S , DO N OT u s e p o wer b a t t ery dur in g f

irmw a re up g r a de. 1 . M a ke s ure yo ur c o m p u t er is c o nne c ted t o t he I nt e r ne t . 2 . Ple a s e c l o s e a ll t

he o t her ap p l i c a ti o ns dur i ng t he f i r mw a re up gr a de, in c lud i ng a nti - v i rus s o f t w a re a nd f ire w a ll . 3. M a ke s ure t

he p o w er s upply is s e curely c o nne c t ed. DO NOT u n -p lu g t he p o w er s upply unti l f

irmw a re up gr a de h a s f

in i s hed. 4 . C o nne c t s y s tem t o PC w i t h M i c r o - U S B c ab l e, DO NOT b r e a k c o nn e c ti o n un ti l f i rmw a re up gra de i s f in i s hed. 5. R un S o f t w a re and w a i t f

o r c o nne c ti o n. 6 . S ele c t Up gra de o p t i o n  C h e c k t

he MC and PMU F i r mw a re V e r s i o n . 7. DJI s erver w ill c he c k yo ur cu r r ent f i r mw a re v e r s i o n, a nd g et t he l a t e s t f

i rmw a r e p r ep a red f

o r t he un i t . 8 . I f t here is a f

i r mw a re v e r s i o n m o re u p - t o - d at e t

h an yo ur cur rent v er s i o n, y o u w ill be ab l e t o c li c k to upd a t e t h e m . 9 . W a i t un ti l A ss i s ta nt s o f t w a re s h o w s “f

i ni s hed ” . 1 0. C li c k OK and p o w er c y c le t he un i t a f t er at l e a s t 5 s e c o nd s . 11 . Y o ur un i t is n o w u p - t o - d a te. (1) A f t er f i r mw a re up gr a d e , p l e a s e r e - c o n f i g ure t h e s y s t e m u s i ng A ss i s ta nt s o f tw a re. ( 2 ) I f f

irmw a re up gr a de f

a i le d , t he s y s tem w ill enter w a i ti ng f o r f i rmw a re up gr a de s ta t

us a ut o m a ti c a l l y , p l e a s e t

r y a g a in w i t

h t he ab o v e p ro c e dur e s . (3) S ele c t Up gra de o p t i o n  C h e c k t

he G P S F irm w a re V er s i o n, o nline up gra de is di s a b l e .© 20 1 5 D JI . A l l Rights Re se rv e d . 

### 25 | 

## L E D D e s c ri p ti o n S y s t e m 

### S t at

u s LED F l a s h in g S y s t e m s ta rt a nd s el f

- c h e c k I MU abn o rm a l d at a o r need a dva n c ed c a libr a ti o n* Wa rm up a f

t er p o w er o n T he a i r c r a f

t is m o v ed o r b i a s o f s en so rs t o o b ig C o m p as s er r o r t o o b i g , need re c a libr a ti o n. T r a n s mi t ter ( T X ) s i g n a l l o s t , ent er t he F a i l S a f

e. T X s ti c k ( s ) mi d p o i nt err o r t o o big Lo w vo l t a g e a lert o r o t her abn o rm a l a ler t * (e . g . C o n f

i g ur a ti o n err o r, T X d a

t a er r o r, En ab l e l o w vo l t a g e p ro te c ti o n w i th o ut PM U , S N er r o r o r C o m p as s abn o rm a l w o rk . ) R e c o rd f o rw a rd dire c ti o n o r h o m e p o i nt

C o nt r o l M o de Ind i c to r M a nu a l M o d e : N o ne ATT I . M o d e : ( s ti c k ( s ) n o t at c en ter ) GPS M o de : ( s ti c k ( s ) n o t a t c ent er ) I OC M o de : ( s ti c k ( s ) n o t at c en ter ) GPS S i g n a l is B e s t ( GPS S at e l li t e nu m ber > 6 ) : N o ne GPS S i g n a l St a t e I ndi c a to r GPS S i g n a l is W ell ( GPS S a tell i t e nu m ber = 6 ) : ( GP S / C o mp a s s M o dule is ne c e ss a ry ) GPS S i g n a l is Ba d ( GPS S a tell i t e nu m ber = 5 ) : GPS S i g n a l is Wo r s t ( GPS S a tell i t e num b e r < 5 ) : 

## C o mp a ss C a l i b ra t i on LED F l a s h in g

B eg in h o ri z o nt a l c a libr a ti o n B eg in v ert

i c a l c a libr a ti o n C a libr a ti o n o r o thers er

r o r

* Y o u c a n f

i g ure o ut t

he er r o r by c o nne c ti ng t

he aut o pil o t s y s t em t o t

he a ss i s t a nt s o f

t w a r e .© 20 1 5 D JI . A l l Rights Re se rv e d . 

### 26 | accessible d software

onnec t ion take positive power supply **M 1**  **M 2**  **M3 ESC**  **M 4**  **M 5**  **M 6**  

# I n s t r u c tion of V 1 **(** a l s o kno wn a s NAZ A - M ) V 1 ( a l s o k n o wn a s N A Z A - M) s y s t em is di ff erent f r o m V2 s y s te m , if yo u a re V 1 s y s t em u s er, p l e a s e re a d t he f o ll o w i ng t e x t c a ref u ll y , a nd refer t o t

he o t her te x t in t

h i s Gui de f

o r u s a g e de ta i ls ( i n c l u ding A ss i s ta nt S o f t w a re C o n f

i g u r a ti o n , B a s i c f l y in g , A d v a n c ed F un c ti o n Ap p e ndix and FA Q, e tc . ) . 

## V 1 A ss e mb ly a

n d C o nn e c t i o n C o nne c t t

he V 1 s y s t em a c c o rd i ng t o t he f o ll o w i ng c h a rt . **R/C System**  Thes e ar e exampl e connections . P l e a s e s e t u p A i l e r o n , E l e v a t o r , Throttle , Rudde r channel s o n you r T X f i r s t , a n d c h o o s e o n e 3 - positions switch/channel a s contro l mod e switch , the n connec t you r receiver to the right ports on MC. **TO B**  **a tt**  **e r**  **y VU**  · D o no t mo un t i t o n an y othe r electroni c devices . M ake sure Yo u can see the LED light during the flight. · I f us e wit h DJ I multi - rotor , yo u ca n solde r th e V U powe r cabl e t o power pads on frame bottom board. Please refer to DJI multi - rotor manual for details. · I f us e wit h 3 r d par t mu lti - rotor , yo u ca n ma k e a connecte r b y yourself to connect VU, ESCs and battery. · Sufficient air flow over the VU is highly recommended. **3 -**  **position switch channe l**  **R/C Receiver (JR)**  **RUDD**

**ELEV AILE**  **THRO 1**  **R/C Receiver 2**  **3 (Futaba / Hitec)**  **4 3**  **- position switch channe**  **l Futaba S**  **- Bus**  **/S -**  **Bus2 S**  **- Bus**  **ESCs, Motors** · Motors and ESCs in DJI multi - rotor kit are recommended. · P l e a s e m a k e s u r e y o u a r e u s i n g t h e E S C s a n d m o t o r s recommended by the manufacturer of your multi rotor first. NAZA output is 400Hz refresh frequency. · I f yo u us e 3 r d part y ESCs , pleas e mak e sur e th e ESC s trave l midpoin t i s a t 152 0 us . D O NO T us e 700u s trave l midpoin t ESC , a s i t ma y lea d aircraf

t t o fl y awa y o r caus e injur y an d damage . Afte r connec t ESC s t o motors , calibrat e al l you r ESC s on e b y on e throug h th e receive r directl y befor e connec t the m t o you r MC , Mak e sur e progra m al l o f t he m in t o G overno r o ff , Brea k o ff an d Normal Start up to get best experience. **I m**  **p o**  **r t**  **a n**  **t :**  the c o nt i nu o u s **PPM PPM**  **Aircraft N**  **o s**  **e Pitch**  **F2 Roll** 
**F1** output of the V U is 3A@5V , a n d the m ax i m u

m i n s t a nt current is 7.5A. If the V U cannot afford the w o r ki n g current for y o u r s e rv o s , p l e a s e use a n i n de p e n de nt power s u pp l y ; o t h e r

w i s e , it may cause the V U safeguard a n d l e a d to the m a i n c o ntr o ll e r r e boo t . **(Optional) GPS/COMPASS**  · GPS/Compass i s s e n s i t i v e to m a gn et i c i nt e r fe r e n c e , s houl d be f a r away f r o m any e l e c t r oni c d e v i c e s . · Yo u s hou l d us e e poxy r e s i n AB g l u e t o a ss e m b l e th e GP S bracke t f i r s t a s th e f

i gu r e showe d i n p r e v i ou s page. · Mount th e bracke t on the center p l a t e o f c r a f t f i r s t , the n fi x th e GP S o n th e p l a t e o f th e bracke t ( b y 3 M g l u e p r o v i d e d ) . The GPS i s s e n s i t i v e to v i b r a t i on i nt e r f e r e n c e , so po s i t i on the bracke t at l ea s t 10 cm f r o m any rotor. · The D J I l ogo marked on the GPS s hou l d f a c e the sk y, w i t h the o r i e nt a t i on arrow po i nt i ng di r e c t l y f o rw a r d. The GPS/Compass i s packaged w i t h a s p e c i a l i ndi c a t i on li n e for m ount i ng for the f i r s t t i m e . · If you are un c e r t a i n whether m a t e r i a l s near the GPS/Compass m odul e are m a gn e t i c or not, you can use a compass or ma gnet to check i t . I f yo u us e you r ow n m oun t i n g rod , mak e sur e i t i s N O T m a gn e t i c ! **MC** · Pleas e us e 3M g ummed pap er provide d T o moun t MC , an d moun t MC parallel to the aircraft horizon. · Th e outpu t port s o f M C (th e righ t sid e i n figure ) shoul d poin t t o th e fron t o f multi - rotor . You ’ d bette r pu t M C a t th e gravit y cente r o f multi - rotor . Please make sure all ports are when installing the MC so as to facilitate wiring an configuration. · In three - pin ports, pins near the nicks are signal pins. · After choosing a location to mount the MC, it is · re commended that you DO NOT mount the MC · until all wirings and software configurations are completed. 

## V 1 i s c o mp at ib le wi th th e P M U V 2 ( A c c e ss ory o f N a za - M V 2 ) V 1 s y s t em is c o mp a tib l e w i t h t he PMU V2 o f V2 s y s te m ; p l e a s e c arry o ut t he f o ll o w i ng c o nne c ti o n. T he o ther m o dules c o nn e c ti o n is t

he s a me a s bef

o re. I m p o rta n t : Y o u a re a s ked t o up gr a de yo ur F irmw a re v er s i o n o f V 1 MC t o V 3 . 1 0 o r ab o ve, a s t he P UM V2 c an o nly w o rk w i t h t he MC o f v er s i o n 3 . 1 0 o r a b o v e.

Take nega t ive power supply Disc© 20 1 5 D JI . A l l Rights Re se rv e d . 

### 27 | 

## V 1 P o rt D e s c ri pt i o n Ple a s e re m ember t

he f un c ti o n o f e a c h p o rt, wh i ch ma y h e lp yo u t o u s e t he Na z a - M e f

f i c i ent ly . 

## Mai n C o n t

r o ll e r **A** F o r r o ll c o nt

r o l (le f t / r i g ht) **E** F o r pi tch c o nt r o l ( f r o nt/b a c k) **T** F o r t

hr o ttle c o nt

r o l **R** F o r ru d der c o nt r o l **U** F o r C o nt

r o l M o de S w i tc h **X1** F o r g i m

b a l pi t c h c o nt r o l Or f o r g a in t un i ng **X2** F o r D - B us ( S - B u s / S - B u s 2 c o mp a ti b l e) Or f o r g a in t un i ng Or f

o r I OC s w i t c h **X3** F o r v o l t a g e m o n i t o r ( C o nn e c t w i t h VU V - S EN p o rt) 

### M1 T o # 1 r o to r 

### M2 T o # 2 r o to r 

### M3 T o # 3 r o to r 

### M4 T o # 4 r o t o r 

### M5 T o # 5 r o to r 

### M6 T o # 6 r o t o r 

### F1 T o g i m

b a l r o ll s er v o Or t o # 7 r o t o r ( Up gra de t he MC F irm w a re t o V 3 . 1 0 o r ab o v e) 

### F2 T o g i m

b a l pi t ch s er v o Or t o # 8 r o t o r ( Up gra de t he M C F i r mw a re t o V 3 . 1 0 o r ab o v e) **LED** L ED p o rt, f

o r L ED w i re c o nn e c ti o n f r o m V er s a ti l e U n i t **EXP.** GPS p o rt , f

o r GPS m o dule w i r e c o nn e c ti o n. ( I n t hre e -pin p o rt s , pins ne a r t he n i cks are s i g n a l pin s . ) 

## V e r s a t i l e Un i t V - S EN V - S EN p o rt : T o t he X 3 p o rt o f the m a in c o nt r o ll er, f o r m o n i t o ring b at tery v o l t a g e a nd s upp lyi ng p o w er  Or ange w i re ( s i g n a l w i re) o ut put : ± ± 3 . 3 V  R ed w i re (p o w er w ire) o utp u t : 3 A @ 5V L ED L ED w ire, t o L ED p o rt o f t he m a in c o n t

r o ll er. U S B p o rt : PC c o nne c ti o n f o r c o n f i g ur a ti o n a nd f

irmw a re up gr a de s . 

## O p t i o n a l GP S & C o mp a ss

C o nne c t t o t

he E X P. p o rt .

## V 1 S p e c i f i c a ti o n G e n e ra l  Three M o des o f Auto pil o t B u i l t- I n F un c ti o ns  Enh an c ed F a il S a f e  L o w Vo l t a g e P r o te c ti o n  S - B u s / S - B u s 2 R e c e i ver S upp o rt  PPM R e c e i v e r S upp o r t  2 - ax le Gi m

b a l S upp o rt 

## P e rip h er a l  Qu a d - r o t o r I 4 , X 4 ;  H e xa - r o t o r I 6 , X 6 , I Y 6 , Y 6 . S upp o rt ed Mul ti - r o t o r  O ct o - r o t o r I 8 , V8 , X 8 ( Up gra de the MC F irm w a re to V 3 . 1 0 o r a b o v e) S upp o rt ed E S C o ut

p u t 4 0 0 H z refre s h f r e quen c y . R e c om m end e d T r a n s mi tt er P CM o r 2 . 4 G Hz w i t h a min i m um 4 c h a nnel s . A ss i s ta n t S o f

t w a r e S y s t em R e q

u i r e ment W i nd o w s XP S P3; W i nd o w s 7 

## E l e c tri c a l & M e c h an i c a l  M C : 4 . 8 V ~ 5 . 5 V W o rki ng V o l t a g e R ange  VU I npu t : 7 . 2 V ~ 2 6 . 0 V (re c o mm e nd 2 S ~ 6 S L i P o ) Out put ( V - S EN p o r t red w ir e ): 3 A @ 5V Out p u t ( V - S EN p o rt red w i r e )bur s t c urr e n t : 7 . 5A P o w e r C o n s u m p t

i o n  MAX : 1 . 5 W ( 0 . 3 A @ 5 V )  N o rm a l: 0 . 6 W ( 0 . 1 2 A @ 5 V) O p er a ti ng T e m

p er at ure - 1 0 ° C ~ 50 ° C ( 1 4 F ~ 1 22 F )  M C : 2 5g W e i gh t  GP S : 2 1 . 3g  VU : 2 0g  M C : 4 5 . 5 m

m × 31 . 5 m m × 1 8 . 5 m m D i m en s i o ns  GPS & C o mp a ss : 4 6 m m (d i am e t er) x 9m m  VU : 3 2 . 2 mm × 2 1 . 1 mm × 7 . 7 mm 

## F l i g ht P er f

o r m a n c e ( c a n be e ff

e ct ed by m e c h a n i c a l pe r f o rm an c e a nd p a y l o a d s ) H o v ering A c curac y (G P S M o de)  V ert i c a l: ± ± 0 . 8 m  H o ri z o nt a l: ± ± 2 . 5m M ax Y aw Angul ar V el o c i t y 2 0 0 ° / s M ax T ilt Angle 4 5° M ax A s c en t / De s c ent Speed ± 6 m / s © 20 1 5 D JI . A l l Rights Re se rv e d . 

### 2 8 |© 20 1 5 D JI . A l l Rights Re se rv e d . 

### 29 | 

# F AQ Ab n o rm a l LE D In d i c ati o n L i st Dur i ng t he C he c ki ng P r o c e dure, if abn o rm a l L ED I ndi c a to r oc curs o r e v en t h e s y s t em c ann o t w o r k n o rm a ll y , p l e a s e refer t o t he f o ll o w i ng li s t and a i ds t

r o ubl e s h o o ti ng . (1) “ S y s t em in i ti a liz i ng a nd s el f - c h e c ki ng LED f

l a s he s ” a re n o t c o r

r e c t ( R ed LED ap p e a rs in t

he l a s t f o ur green f

l a s he s ). T he aut o pil o t s y s t em w o rks abn o r m a ll y . Ple a s e c o ntac t y o ur de a ler . ( 2 ) L ED b l in k s Yell o w 4 ti m es qu i ck l y ( ) . T he s y s t em is w a rm i ng up. Y o u c ann o t s t a rt t he m o t o rs un ti l t he 4 r apid y ell o w f

l a s hes di sap p e a r. I f t

he wa rm up w a i ti ng is l o nger t h an 2 mi nu t e s , p l e a s e p o wer o f f f o r 5 minu te s , c o ld s ta rt , a nd then c o nne c t t he a ss i s ta nt s o f

t w a re, en t er t

he " T oo l s " - > I MU c a libr a ti o n, c a rr y o ut t he Ad va n c ed c a libr a ti o n. (3) A f t er t he s y s t e m s t art and s el f - c he c ki n g h a s f

in i s hed, if t

he LED b l i nk s R ed, Green and Yell o w ( ) c o ntinu a ll y . S en so r er

r o r is t o o big. Ple a s e c o nne c t t he a ss i s ta nt s o f

t w a re, ent er t

he " T oo l s " - > I MU c a libr a ti o n, c a rr y o ut c a libr a ti o n. ( 4 ) A t t he f i r s t m o t o rs s ta rt , t

he s y s t em w ill c h e c k the s en so rs B i a s a nd yo u a re a s ked t o keep t he a i r c r a f

t s ta ti o n a ry (no need o f h o ri z o nt a l le vel). I f yo u c a nn o t s ta rt t he m o t o rs and t

he L ED b l i nk s Green 6 ti m es qu i ckl y ( ), i t m e a ns t h at t he s en so r err o r is t o o big. Ple a s e c o nn e c t t he a ss i s ta nt s o f

t w a re, enter t he " T oo l s " - > I MU c a libr a ti o n, c a rry o ut b a s i c c a libr a ti o n. N o t e: a f t er t he f i r s t s u cc e ssf

ul m o t o rs s ta rt , t

h i s c h e c k in g w ill be di sab l ed and i t is no need any m o re to keep t he a i r c r a f t s ta ti o n a ry dur i ng s ta r ti ng m o t o r s . (5) T he s y s t e m b l in ks R ed LE D qu i ckl y dur i ng f l y ing. L o w - v o l t a g e p ro t e c ti o n is t rig g ere d. Ple a s e l and t

he a i r c r a f t A S AP. ( 6 ) The s y s t e m b l in k s Ye l l o w L ED qu i ck ly dur in g f l yin g . F a i l S a f

e M o de is trig g ere d . P a y a tte n ti o n t h a t there i s no t a ll buildings and t

rees t o b l o c k yo ur a i r c r a f t dur i ng g o - h o m e . (7) The L ED b l in k s R ed and Yell o w a l t ern at e l y ( ). C omp as s er r o r is t o o big. a ) T here m a y be a f

er ro m a g n e ti c s ub s t an c e c l o s e t o t he Ph a nto m . L i f

t t he a i r c r a f t up ab o ut 1 m f

r o m t he gr o und, if t

her e is no R ed and Yell o w f l a s h i ng , t hen i t w ill n o t a ff

e c t t he f li g ht . b) O t herw i s e , r e - c a libr a t e t

he c o m p a ss . c ) I f re - c a libr a ti o n d o es n o t w o rk , p l e a s e c o nn e ct t o t he A ss i s ta nt S o f

tw a r e , s ele c t t

he “ T oo l s ” a nd f o ll o w t he ti ps t o c a rry o ut t

h e re q u i red o pe r a ti o n. 

## F i x th e TB E ( T o i l e t Bowl E f f e c t) P r o b l e m When f l ying in GPS A T TI . M o de and t h e c omp as s c a libr a ti o n h a s been d o ne c o rr e c t ly , s h o ul d yo u f i nd t he a i r c r a f

t r o ta ti ng ( T o i let b o w l e f

f e c t ), o r dr i f ti ng when h o v eri n g . P le a s e c h e c k t he G P S m o dule m o un ti ng o rient a ti o n a nd t h e n re - do t he c o m p as s c a libr a ti o n. C a rry o ut t h e f o ll o w i ng p r o c edure t o r e - m o unt t he GPS m o dul e.© 20 1 5 D JI . A l l Rights Re se rv e d . 

### 30 | l o c k w i s e r o ta is t he r o ta ti ng dire c ti o n o f a i r c r a f t , a rr o w dire c ti o n o n t

he G P S m o dule, θ is t

he o ti ng GPS re - m o un ti ng C

θ nt er C l o c k w i s e i o n o f a i r c r a f

t , PS r e - m o un ti ng ( a b o ut 1 0~ 3 0 o ) r o ta ti ng GPS re - m o un ti ng θ I n t he f o ll o w i ng di a gr am ( v iew f r o m t he t o p), t

he a i r c r a f

t c a n ap p e a r t o be r o ta ti ng in b o t h c l o c k w i s e a nd c o unt er - c l o c k

w i s e dire c ti o n, p l e a s e r e - m o u n t t he G P S m o dule c o rr e s p o nding l y .

i s t he n o s e dire c t is t h e ffs et angle f o r G C o



## S h o u ld y o u f

in d t h e m u l ti - r o t o r d o e s n o t t

r ac k s tra i gh t i n f

o rw ar d fl i g ht . Ple a s e c a r

ry o ut s e v er a l m o re c o ur s e s , t he s y s t e m w ill f

ix i t a uto m a ti c a ll y . 

## M o t o r s S tar

t f ai l ur e c au s e d b y TX s t i c k ( s) m i d - p o int e rror t o o b i g I f t he T X s ti c k ( s ) mi d - p o i nt err o r is t o o big, M o t o rs Sta rt w ill f a il when yo u e x e cute t he C o m bin a ti o n S ti c k C om m ands ( C S C ) and le a d t o t he a ir c r a f

t w ill n o t ta ke o ff

. . And t he LED w ill b l ink R ed f o ur ti m es per s e c o nd c o ntinu a ll y t o w a rn yo u. T X s ti c k ( s ) mi d - p o i nt err o r t o o big c an be c au s ed by t he f o ll o w i ng re a s o n s : (1) There is T X s ti c k (e x c e pt t h e t hro t tle s ti c k) n o t at c en ter w hen p o w er o n t

he aut o pil o t s y s t e m . ( 2 ) T he T X s ti c ks h a s been t r i mm e d, w h i ch le a d s t o t he l ar g e d e v i a ti o n o f mi d - p o i nt . F o r e xa m p le, t he S UB - T RI M h a s been a dju s t ed f o r F ut aba t

r a n s mi t t er. (3) The T X s ti c k ( s ) t

r a v el h a s l a r g er a s ym m e t r y . F o r t he re a s o n ( 1 ), p l e a s e put a ll T X s ti c k s a t t h e mi d - p o i nt , a nd t

hen p o w er c yc le t

he aut o pil o t s y s t e m t o r e - re c o r d t he mi d - p o i nt . I f t

he p r o b l em c o n ti nue s , t

h at c a n be c au s ed by t

he re a s o n ( 2 ) o r re a s o n (3 ) , yo u need t o a dju s t t he o ut put range o f yo ur T X , a nd t h e n u s e t

he A ss i s ta nt S o f

t w a re t o re d o t

h e T X c a libr a ti o n. Ple a s e c a r ry o u t t he f o ll o w i ng p ro c edur e s . (1) C o nne c t t o t

he A ss i s ta nt s o f

t w a re, c li c k B a s i c - > R/ C - > C o mm a n d S ti c k s C a libr a ti o n, a nd p u s h a ll T X s ti c k s t h r o ugh o ut t

he i r c o m p l e t e t ra v el r a nge t o s ee if a ny s ti c k c a nn o t r e a ch i t s l a r g e s t p o s i ti o n. ( 2 ) A dju s t t

he l a rg e s t t

ra v el o f T X s ti c k unti l t

he cur s o r o n t

he A ss i s ta n t s o f

t w a re c an re a c h b o t

h e nd p o s i ti o n s , a cc o rd i ng t o yo ur T X m a nu a l. (3) P o wer c y c le t

he aut o pil o t s y s t e m , n o t e t h at p o w er c y c le is re qu i re d . ( 4 ) Redo t

he T X c a libr a ti o n a cc o rd i n g t o t he A ss i s ta nt s o f

t w a re.© 20 1 5 D JI . A l l Rights Re se rv e d . 

### 31 | r o du c t s , t hen a DJI C A

N HU B m o dule i s 

## A tt it u d e C o n tr o l l ab le W

h e n O n e M o t o r O utput i s F a i l e d F o r H e x a - r o t o r, in c lud in g H e x a - r o t o r I , H e x a - r o t o r V , H e xa - r o t o r I Y a nd H e x a - r o t o r Y, a i r c r a f t is a tti t u d e c o nt r o ll ab l e when o ne m o t o r o ut

put is f a i le d . T he N AZ A - M c a n s ti l l c o n t r o l t he a tti t ude o f t he H e xa - r o t o r f

o r a s a f e l a nding w

hen o ne m o t o r o ut

p u t o f t h e H e xa - r o t o r h a s f

a i le d , f o r e x a m p l e, o ne m o t o r is s to p p ed o r o ne p ro pe l l er is b r o ken, e t c . T he c o nt r o l m o de o f NAZ A - M s h o uld be in A t ti . M o de o r G P S A t ti . M o d e . T he a i r c r a f t w ill r o ta t e , due t o an i mb a l a n c e o f t o r q

ue; h o w e v e r , i t c a n s ti ll be c o n t r o ll ed by t

he T r a n s mi tt e r . S ele c t C o ur s e l o c k o r h o me l o c k m o de f o r f l ying t he a i r c r a f

t i nt o a s a f

e a rea t o l a nd w

hen t he a i r c r a f t is f a r a w a y o r t he a tti t ude c a n ’ t be r e c o g n i ze d . E v en w h e n t he m ul ti r o t o r is r o ta ti ng , u s i n g C o ur s e l o c k o r h o m e l oc k m o de w i l l a ll o w yo u t o m o v e t

he m u l ti r o t o r in t

he c o rr e s p o ndi n g T r a n s mi tter s ti c k dir e c t i o n . 

## Wh en u s e d w i t

h o th e r D J

I p r o d u c t s T he N A Z A - M s y s t e m c om m un i c at es w i t

h o t her DJI p r o du ct s (e . g . H 3 - 2 D g i mb a l, B T U m o dule, i O S D mini a nd i O S D M a rk II ) v ia t

he C A N - B us p o rt ( ) o f t

he N AZA PMU V2 . Y o u c a n p lug n e w DJI p r o du c t s in t o a ny s p are C A N - B u s p o rt, s in c e C A

N - B us p o r

t s o n N A ZA - M, C A

N HUB , G C U , i O S D m in i , i O S D M a rk I I and 2 . 4 G B luet oo t h D a t a link a re t he s a me f

o r t he c o m m un i c a ti o n s . When t here a re n o t en o ugh CA N - B us p o rt s f

o r a d d i ti o n a l DJI re c om m end e d. The f

o ll o w i ng di a gr am is f

o r yo ur c o nne c ti o n refere n c e.

F i g . 1 U s ed w i t

h i O S D M a rk I I© 20 1 5 D JI . A l l Rights Re se rv e d . 

### 32 | h C AN HU B F i g . 2 U s ed w i t

F i g . 3 U s e a CA

N H U B t o c o nn e c t t

h e 2 . 4 G B lue t oo t

h D ata li n k U s ers c a n u s e t

he NM A ss i s ta nt o n t

he m o bile de v i c e when a B TU m o du le is c o nne c ti ng w i t h t he Gr o und end o f the 2 . 4 G B lue t oo t h D ata link (No need t o c o nne c t an o t her B TU m o dule t o t

he F light c o nt r o l s y s t e m) .