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Volumn 7436 LNCS, Issue , 2012, Pages 252-266

Satellite rendezvous and conjunction avoidance: Case studies in verification of nonlinear hybrid systems

Author keywords

[No Author keywords available]

Indexed keywords

AUTOMATIC VERIFICATION; AUTONOMOUS OPERATIONS; FORMAL VERIFICATIONS; HUMAN OPERATOR; NOISY SENSORS; ORBITAL DYNAMICS; ORBITAL PARAMETERS; PROTOTYPE TOOLS; QUOTIENTING; RELIABILITY ASSURANCE; RELIABILITY CRITERION; SATELLITE SYSTEM; STATE-SPACE; SYSTEMS MODELS;

EID: 84865989672     PISSN: 03029743     EISSN: 16113349     Source Type: Book Series    
DOI: 10.1007/978-3-642-32759-9_22     Document Type: Conference Paper
Times cited : (14)

References (22)
  • 2
    • 62949169899 scopus 로고    scopus 로고
    • Reachability analysis of nonlinear systems with uncertain parameters using conservative linearization
    • December
    • Althoff, M., Stursberg, O., Buss, M.: Reachability analysis of nonlinear systems with uncertain parameters using conservative linearization. In: 47th IEEE Conference on Decision and Control (CDC), pp. 4042-4048 (December 2008)
    • (2008) 47th IEEE Conference on Decision and Control (CDC) , pp. 4042-4048
    • Althoff, M.1    Stursberg, O.2    Buss, M.3
  • 6
    • 33846672502 scopus 로고    scopus 로고
    • Hybridization methods for the analysis of nonlinear systems
    • Asarin, E., Dang, T., Girard, A.: Hybridization methods for the analysis of nonlinear systems. Acta Informatica 43, 451-476 (2007)
    • (2007) Acta Informatica , vol.43 , pp. 451-476
    • Asarin, E.1    Dang, T.2    Girard, A.3
  • 8
    • 0003738441 scopus 로고    scopus 로고
    • An introduction to the mathematics and methods of astrodynamics
    • American Institute of Aeronautics and Astronautics
    • Battin, R.H.: An introduction to the mathematics and methods of astrodynamics. AIAA education series. American Institute of Aeronautics and Astronautics (1999)
    • (1999) AIAA Education Series
    • Battin, R.H.1
  • 12
    • 24344447320 scopus 로고    scopus 로고
    • PHAVer: Algorithmic Verification of Hybrid Systems Past HyTech
    • Morari, M., Thiele, L. (eds.) HSCC 2005. Springer, Heidelberg
    • Frehse, G.: PHAVer: Algorithmic Verification of Hybrid Systems Past HyTech. In: Morari, M., Thiele, L. (eds.) HSCC 2005. LNCS, vol. 3414, pp. 258-273. Springer, Heidelberg (2005)
    • (2005) LNCS , vol.3414 , pp. 258-273
    • Frehse, G.1
  • 13
    • 79960348872 scopus 로고    scopus 로고
    • SpaceEx: Scalable Verification of Hybrid Systems
    • Gopalakrishnan, G., Qadeer, S. (eds.) CAV 2011. Springer, Heidelberg
    • Frehse, G., Le Guernic, C., Donzé, A., Cotton, S., Ray, R., Lebeltel, O., Ripado, R., Girard, A., Dang, T., Maler, O.: SpaceEx: Scalable Verification of Hybrid Systems. In: Gopalakrishnan, G., Qadeer, S. (eds.) CAV 2011. LNCS, vol. 6806, pp. 379-395. Springer, Heidelberg (2011)
    • (2011) LNCS , vol.6806 , pp. 379-395
    • Frehse, G.1    Le Guernic, C.2    Donzé, A.3    Cotton, S.4    Ray, R.5    Lebeltel, O.6    Ripado, R.7    Girard, A.8    Dang, T.9    Maler, O.10
  • 14
    • 33747031710 scopus 로고    scopus 로고
    • Manifolds and metrics in the relative spacecraft motion problem
    • Gurfil, P.,Kholshevnikov, K.V.: Manifolds and metrics in the relative spacecraft motion problem. Journal of Guidance Control and Dynamics 29(4), 1004-1010 (2006)
    • (2006) Journal of Guidance Control and Dynamics , vol.29 , Issue.4 , pp. 1004-1010
    • Gurfil, P.1    Kholshevnikov, K.V.2
  • 19
    • 67649321654 scopus 로고    scopus 로고
    • Rational billiards and flat structures
    • Hasselblatt, B., Katok, A. (eds.) ch. 13, Elsevier Science
    • Masur, H., Tabachnikov, S.: Rational billiards and flat structures. In: Hasselblatt, B., Katok, A. (eds.) Handbook of Dynamical Systems, Handbook of Dynamical Systems, vol. 1 Part A, ch. 13, pp. 1015-1089. Elsevier Science (2002)
    • (2002) Handbook of Dynamical Systems, Handbook of Dynamical Systems , vol.1 , Issue.PART A , pp. 1015-1089
    • Masur, H.1    Tabachnikov, S.2
  • 20
    • 3042833856 scopus 로고    scopus 로고
    • Finite burn maneuver modeling for a generalized spacecraft trajectory design and optimization system
    • Ocampo, C.: Finite burn maneuver modeling for a generalized spacecraft trajectory design and optimization system. Annals of the New York Academy of Sciences 1017(1), 210-233 (2004)
    • (2004) Annals of the New York Academy of Sciences , vol.1017 , Issue.1 , pp. 210-233
    • Ocampo, C.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.