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Volumn 13, Issue 3, 2009, Pages 209-220

Pitch and roll attitude estimation of a small-scaled helicopter using single antenna GPS with gyroscopes

Author keywords

Attitude estimation; GPS; Unmanned helicopter

Indexed keywords

ACADEMIC LABORATORY; ANGULAR RATE; ATTITUDE ESTIMATION; COMPLEMENTARY FILTERS; ESTIMATION ALGORITHM; GPS; ONBOARD COMPUTERS; PITCH ATTITUDE; POST PROCESSING; RADIO-CONTROLLED MODELS; RC HELICOPTER; REFERENCE SYSTEMS; RESEARCH PLATFORMS; SINGLE ANTENNA; SINGLE-ANTENNA GPS RECEIVERS; UNMANNED HELICOPTER; VELOCITY INFORMATION;

EID: 70350000605     PISSN: 10805370     EISSN: 15211886     Source Type: Journal    
DOI: 10.1007/s10291-008-0114-z     Document Type: Article
Times cited : (17)

References (19)
  • 1
    • 0032715403 scopus 로고    scopus 로고
    • Satellite attitude determination based on GPS signal-to-noise ratio
    • Axelrad P, Behre CP (1999) Satellite attitude determination based on GPS signal-to-noise ratio. Proc IEEE 87(1):133-144.
    • (1999) Proc IEEE , vol.87 , Issue.1 , pp. 133-144
    • Axelrad, P.1    Behre, C.P.2
  • 2
    • 27744503592 scopus 로고    scopus 로고
    • Brown AK (2005) GPS/INS uses low-cost MEMS IMU. IEEE A E Syst Mag:3-10
    • Brown AK (2005) GPS/INS uses low-cost MEMS IMU. IEEE A E Syst Mag:3-10.
  • 3
    • 35648954622 scopus 로고    scopus 로고
    • Cho A, Kim J, Lee S et al. (2007) Fully automatic taxiing, takeoff and landing of a UAV only with a single-antenna GPS receiver. In: AIAA Infotech at Aerospace 2007 Conference and Exhibit
    • Cho A, Kim J, Lee S et al. (2007) Fully automatic taxiing, takeoff and landing of a UAV only with a single-antenna GPS receiver. In: AIAA Infotech at Aerospace 2007 Conference and Exhibit.
  • 4
    • 0031199019 scopus 로고    scopus 로고
    • GPS for low-cost attitude determination a review of concept, in-flight experiences, and current developments
    • Chu QP, van Woerkom PTLM (1997) GPS for low-cost attitude determination a review of concept, in-flight experiences, and current developments. Acta Astronaut 41(4):421-433.
    • (1997) Acta Astronaut , vol.41 , Issue.4 , pp. 421-433
    • Chu, Q.P.1    van Woerkom, P.T.L.M.2
  • 5
    • 0028383252 scopus 로고
    • Flight tests of attitude determination using GPS compared against an inertial navigation unit
    • Cohen CE, McNally BD, Parkinson BW (1994) Flight tests of attitude determination using GPS compared against an inertial navigation unit. Navigation 41:83-97.
    • (1994) Navigation , vol.41 , pp. 83-97
    • Cohen, C.E.1    McNally, B.D.2    Parkinson, B.W.3
  • 6
    • 70349993775 scopus 로고    scopus 로고
    • Collinson RPG (1996) Introduction to avionics, 1st edn. Microwave Technology Series 11. Chapman & Hall, London
    • Collinson RPG (1996) Introduction to avionics, 1st edn. Microwave Technology Series 11. Chapman & Hall, London.
  • 7
    • 70349985398 scopus 로고    scopus 로고
    • Conway AR (1995) Autonomous control of an unstable model helicopter using carrier phase GPS only. Ph.D. thesis, Stanford University
    • Conway AR (1995) Autonomous control of an unstable model helicopter using carrier phase GPS only. Ph.D. thesis, Stanford University.
  • 8
    • 70349992536 scopus 로고    scopus 로고
    • Evans J, Hodge W, Liebman J et al. (1999) Flight tests of an unmanned air vehicle with integrated multi-antenna GPS receiver and IMU: towards a testbed for distributed control and formation flight. In: Proceedings of the ION-GPS Conference. Nashville
    • Evans J, Hodge W, Liebman J et al. (1999) Flight tests of an unmanned air vehicle with integrated multi-antenna GPS receiver and IMU: towards a testbed for distributed control and formation flight. In: Proceedings of the ION-GPS Conference. Nashville.
  • 9
    • 0034481792 scopus 로고    scopus 로고
    • Gavrilets V, Shterenberg A, Dahleh MA et al. (2000) Avionics system for a small unmanned helicopter performing aggressive maneuvers. In: The 19th Digital Avionics Systems Conference, vol. 1. Philadelphia, PA
    • Gavrilets V, Shterenberg A, Dahleh MA et al. (2000) Avionics system for a small unmanned helicopter performing aggressive maneuvers. In: The 19th Digital Avionics Systems Conference, vol. 1. Philadelphia, PA.
  • 10
    • 70349999577 scopus 로고    scopus 로고
    • Gavrilets V, Mettler B, Feron E (2003) Dynamic model for a miniature aerobatic helicopter. Tech. Rep. LIDS-P-2580, MIT-LIDS
    • Gavrilets V, Mettler B, Feron E (2003) Dynamic model for a miniature aerobatic helicopter. Tech. Rep. LIDS-P-2580, MIT-LIDS.
  • 12
    • 85013598895 scopus 로고    scopus 로고
    • Johnson EN, Fontaine SG, Kahn AD (2001) Minimum complexity uninhabited air vehicle guidance and flight control system. In: Proceedings of the 20th Digital Avionics Systems Conference, vol. 1
    • Johnson EN, Fontaine SG, Kahn AD (2001) Minimum complexity uninhabited air vehicle guidance and flight control system. In: Proceedings of the 20th Digital Avionics Systems Conference, vol. 1.
  • 13
    • 0032021278 scopus 로고    scopus 로고
    • Single-antenna GPS-based aircraft attitude determination
    • Kornfeld RP, Hansman RJ, Deyst JJ (1998) Single-antenna GPS-based aircraft attitude determination. Navigation 45(1):51-60.
    • (1998) Navigation , vol.45 , Issue.1 , pp. 51-60
    • Kornfeld, R.P.1    Hansman, R.J.2    Deyst, J.J.3
  • 14
    • 85085778328 scopus 로고    scopus 로고
    • Lee S, Lee T, Park S et al. (2003) Flight test results of UAV automatic control using a single-antenna GPS receiver. In: AIAA Guidance, Navigation, and Control Conference and Exhibit
    • Lee S, Lee T, Park S et al. (2003) Flight test results of UAV automatic control using a single-antenna GPS receiver. In: AIAA Guidance, Navigation, and Control Conference and Exhibit.
  • 15
    • 29744447116 scopus 로고    scopus 로고
    • Lievens KPA, Muldery JA, Chu P (2005) Single GPS antenna attitude determination of a fixed wing aircraft aided with aircraft aerodynamics. In: AIAA Guidance, Navigation, and Control Conference and Exhibit. San Francisco, California
    • Lievens KPA, Muldery JA, Chu P (2005) Single GPS antenna attitude determination of a fixed wing aircraft aided with aircraft aerodynamics. In: AIAA Guidance, Navigation, and Control Conference and Exhibit. San Francisco, California.
  • 16
    • 0033155596 scopus 로고    scopus 로고
    • Spacecraft attitude/rate estimation using vector-aided GPS observations
    • Oshman Y, Markley FL (1999) Spacecraft attitude/rate estimation using vector-aided GPS observations. IEEE Trans Aerosp Electron Syst 35(3):1019-1032.
    • (1999) IEEE Trans Aerosp Electron Syst , vol.35 , Issue.3 , pp. 1019-1032
    • Oshman, Y.1    Markley, F.L.2
  • 17
    • 29744462805 scopus 로고    scopus 로고
    • Roberts PJ, Walker RA (2005) Fixed wing UAV navigation and control through integrated GNSS and vision. In: AIAA Guidance, Navigation, and Control Conference and Exhibit. San Francisco, California
    • Roberts PJ, Walker RA (2005) Fixed wing UAV navigation and control through integrated GNSS and vision. In: AIAA Guidance, Navigation, and Control Conference and Exhibit. San Francisco, California.
  • 18
    • 84881345128 scopus 로고    scopus 로고
    • Rock SM, Frew EW, Jones H et al. (1998) Combined CDGPS and vision-based control of a small autonomous helicopter. In: Proceedings of the 1998 American Control Conference, Philadelphia
    • Rock SM, Frew EW, Jones H et al. (1998) Combined CDGPS and vision-based control of a small autonomous helicopter. In: Proceedings of the 1998 American Control Conference, Philadelphia.
  • 19
    • 70349984188 scopus 로고    scopus 로고
    • Wang C,Walker RA (2003) Single antenna attitude determination for Fedsat with improved antenna gain patterns. In: Proceedings of the 6th International Symposium on Satellite Navigation Technology. Melbourne, Australia
    • Wang C,Walker RA (2003) Single antenna attitude determination for Fedsat with improved antenna gain patterns. In: Proceedings of the 6th International Symposium on Satellite Navigation Technology. Melbourne, Australia.


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.