• 제목/요약/키워드: pseudo-orbit

검색결과 37건 처리시간 0.028초

HYPERBOLIC STRUCTURE OF POINTWISE INVERSE PSEUDO-ORBIT TRACING PROPERTY FOR C1 DIFFEOMORPHISMS

  • Manseob Lee
    • 대한수학회논문집
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    • 제38권1호
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    • pp.243-256
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    • 2023
  • We deal with a type of inverse pseudo-orbit tracing property with respect to the class of continuous methods, as suggested and studied by Pilyugin [54]. In this paper, we consider a continuous method induced through the diffeomorphism of a compact smooth manifold, and using the concept, we proved the following: (i) If a diffeomorphism f of a compact smooth manifold M has the robustly pointwise inverse pseudoorbit tracing property, f is structurally stable. (ii) For a C1 generic diffeomorphism f of a compact smooth manifold M, if f has the pointwise inverse pseudo-orbit tracing property, f is structurally stable. (iii) If a diffeomorphism f has the robustly pointwise inverse pseudo-orbit tracing property around a transitive set Λ, then Λ is hyperbolic for f. Finally, (iv) for C1 generically, if a diffeomorphism f has the pointwise inverse pseudo-orbit tracing property around a locally maximal transitive set Λ, then Λ is hyperbolic for f. In addition, we investigate cases of volume preserving diffeomorphisms.

LIMIT SETS OF POINTS WHOSE STABLE SETS HAVE NONEMPTY INTERIOR

  • Koo, Ki-Shik
    • 충청수학회지
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    • 제20권3호
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    • pp.343-348
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    • 2007
  • In this paper, we show that if a homeomorphism has the pseudo-orbit-tracing-property and its nonwandering set is locally connected, then the limit sets of wandering points whose stable sets have nonempty interior consist of single periodic orbit.

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EVOLUTION OF ORBIT AND ROTATION OF A PSEUDO-SYNCHRONOUS BINARY SYSTEM ON THE MAIN SEQUENCE

  • Li, Lin-Sen
    • 천문학회지
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    • 제51권1호
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    • pp.1-4
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    • 2018
  • We study the pseudo-synchronous orbital motion of a binary system on the main sequence. The equations of the pseudo-synchronous orbit are derived up to $O(e^4)$ where e is the eccentricy of the orbit. We integrate the equations to present their solutions. The theoretical results are applied to the evolution of the orbit and spin of the binary star Y Cygni, which has a current eccentricity of $e_0\;=\;0.142$. We tabulate our numerical results for the evolution of the orbit and spin per century. The numerical results for the semi-major axes and rotational angular velocities in the evolutional time scales of three stages (synchronization, circularization, and collapse time scale) are also tabulated. Synchronization is achieved in about $5{\times}10^3\;years$ followed by circularization lasting about $1{\times}10^5\;years$ before decaying in $2{\times}10^5\;years$.

CONTINUOUS ORBIT EQUIVALENCES ON SELF-SIMILAR GROUPS

  • Yi, Inhyeop
    • 대한수학회보
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    • 제58권1호
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    • pp.133-146
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    • 2021
  • For pseudo-free and recurrent self-similar groups, we show that continuous orbit equivalence of inverse semigroup partial actions implies continuous orbit equivalence of group actions. Conversely, if group actions are continuous orbit equivalent, and the induced homeomorphism commutes with the shift maps on their groupoids, we obtain continuous orbit equivalence of inverse semigroup partial actions.

TLE를 이용한 우주물체 궤도예측 정밀도 향상 연구 (A Study on Enhancement of Orbit Prediction Precision for Space Objects Using TLE)

  • 임현정;정옥철;정대원
    • 한국항공우주학회지
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    • 제42권3호
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    • pp.270-278
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    • 2014
  • 본 논문에서는 우주물체 궤도예측의 개선 방안에 관하여 기술하였다. 운용위성과 우주물체와의 근접 가능성 여부를 확인하기 위해 이용되는 TLE(Two-Line Element)를 가관측으로 사용하였고, 비행역학시스템을 통해 궤도결정 및 예측을 수행하였다. 궤도를 결정함에 있어 일정기간 내 일련의 TLE를 이용하여 상태벡터를 가정하였고, 결정기간 및 가관측수(pseudo-observations)에 따른 예측결과 오차를 분석하였다. 또한, 제안된 방식을 적용할 경우 궤도예측 정밀도가 향상 되는지를 알아보기 위해 수 미터 수준의 정밀궤도 확인이 가능한 아리랑위성 2, 3호를 대상으로 먼저 적용하였으며, 동일한 조건으로 우주물체에 적용한 결과를 분석하였다. 우주물체 궤도예측의 RMS 오차 비교 결과, 7일 전파기준으로 궤도 예측 정밀도를 약 90% 향상시킬 수 있었다. 우주물체의 개선된 궤도예측은 매일 수행되는 충돌가능성 분석에 이용되어 위험성이 높은 근접 우주물체의 1차적인 선별에 활용가능 할 것이다.

Orbit Determination System for the KOMPSAT-2 Using GPS Measurement Data

  • Lee, Byoung-Sun;Yoon, Jae-Cheol;Kim, Jae-Hoon
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2003년도 ICCAS
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    • pp.2325-2330
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    • 2003
  • GPS based orbit determination system for the KOMPSAT-2 has been developed. Two types of orbit determination software such as operational orbit determination and precise orbit determination are designed and implemented. GPS navigation solutions from on-board the satellite are used for the operational orbit determination and raw measurements data such as C/A code pseudo-range and L1 carrier phase for the precise orbit determination. Operational concept, architectural design, software implementation, and performance test are described.

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AVERAGE SHADOWING PROPERTIES ON COMPACT METRIC SPACES

  • Park Jong-Jin;Zhang Yong
    • 대한수학회논문집
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    • 제21권2호
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    • pp.355-361
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    • 2006
  • We prove that if a continuous surjective map f on a compact metric space X has the average shadowing property, then every point x is chain recurrent. We also show that if a homeomorphism f has more than two fixed points on $S^1$, then f does not satisfy the average shadowing property. Moreover, we construct a homeomorphism on a circle which satisfies the shadowing property but not the average shadowing property. This shows that the converse of the theorem 1.1 in [6] is not true.

THE PSEUDO ORBIT TRACING PROPERTY AND EXPANSIVENESS ON UNIFORM SPACES

  • Lee, Kyung Bok
    • 충청수학회지
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    • 제35권3호
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    • pp.255-267
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    • 2022
  • Uniform space is a generalization of metric space. The main purpose of this paper is to extend several results contained in [5, 6] which have for an expansive homeomorphism with the pseudo orbit tracing property(POTP in short) on a compact metric space (X, d) for an expansive homeomorphism with the POTP on a compact uniform space (X, 𝒰). we characterize stable and unstable sets, sink and source and saddle, recurrent points for an expansive homeomorphism which has the POTP on a compact uniform space (X, 𝒰).