지원사업
학술연구/단체지원/교육 등 연구자 활동을 지속하도록 DBpia가 지원하고 있어요.
커뮤니티
연구자들이 자신의 연구와 전문성을 널리 알리고, 새로운 협력의 기회를 만들 수 있는 네트워킹 공간이에요.
논문 기본 정보
- 자료유형
- 학술저널
- 저자정보
- 저널정보
- 한국항공우주학회 International Journal of Aeronautical and Space Sciences International Journal of Aeronautical and Space Sciences Volume.15 Number.2
- 발행연도
- 2014.6
- 수록면
- 146 - 152 (7page)
이용수
초록· 키워드
오류제보하기
In this paper, a new adaptive nonsingular terminal sliding mode control theory based impact angle guidance law for intercepting maneuvering targets was documented. In the design procedure, a new adaptive law for target acceleration bound estimation was presented, which allowed the proposed guidance law to be used without the requirement of the information on the target maneuvering profiles. With the aid of Lyapunov stability criteria, the finite-time convergent characteristics of the line-of-sight angle and its derivative were proven in theory. Numerical simulations were also performed under various conditions to demonstrate the effectiveness of the proposed guidance law.
목차
Abstract
1. Introduction
2. Problem Formulation
3. Guidance Law Design
4. Simulation Results
5. Conclusion
References
참고문헌 (21)
참고문헌 신청
1. [학술지(정기간행물)] - Nesline, F. W. / 1985 / A new look at classical vs modern homing missile guidance / Journal of Guidance, Control, and Dynamics 4 (1) : 78 ~ 85
2. [단행본] - Zarchan, P. / 1998 / Tactical and Strategic Missile Guidance / American Institute of Aeronautics and Astronautics Publications
3. [학술지(정기간행물)] - Palumbo, N. F. / 2010 / Basic Principles of Homing Guidance / Johns Hopkins APL Technical Digest 29 (1) : 25 ~ 41
4. [학술지(정기간행물)] - Palumbo, N. F. / 2010 / Modern Homing Missile Guidance Theory and Techniques / Johns Hopkins APL Technical Digest 29 (1) : 42 ~ 59
5. [학술지(정기간행물)] - Yang, C. D. / 1998 / Nonlinear H robust guidance law for homing missiles / Journal of Guidance, Control, and Dynamics 21 (6) : 882 ~ 890
2. [단행본] - Zarchan, P. / 1998 / Tactical and Strategic Missile Guidance / American Institute of Aeronautics and Astronautics Publications
3. [학술지(정기간행물)] - Palumbo, N. F. / 2010 / Basic Principles of Homing Guidance / Johns Hopkins APL Technical Digest 29 (1) : 25 ~ 41
4. [학술지(정기간행물)] - Palumbo, N. F. / 2010 / Modern Homing Missile Guidance Theory and Techniques / Johns Hopkins APL Technical Digest 29 (1) : 42 ~ 59
5. [학술지(정기간행물)] - Yang, C. D. / 1998 / Nonlinear H robust guidance law for homing missiles / Journal of Guidance, Control, and Dynamics 21 (6) : 882 ~ 890
이 논문의 저자 정보
최근 본 자료
댓글(0)
0
UCI(KEPA) : I410-ECN-0101-2015-550-002914136