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Volumn 33, Issue 2, 2010, Pages 601-606

Synthetic-waypoint guidance algorithm for following a desired flight trajectory

Author keywords

[No Author keywords available]

Indexed keywords

AIR NAVIGATION; AIR TRAFFIC CONTROL; AIRCRAFT; AIRCRAFT CONTROL; NAVIGATION SYSTEMS;

EID: 77950487084     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.46204     Document Type: Article
Times cited : (79)

References (13)
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    • Practical guidance for homing missiles with bearings-only measurements
    • doi:10.1109/7.481284
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    • Gyu Taek, L.1    Jang Gyu, L.2
  • 9
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    • Line-of-sight rate estimation and linearizing control of an imaging seeker in a tactical missile guided by proportional navigation
    • DOI 10.1109/TCST.2002.1014675, PII S1063653602053563
    • Waldmann, J., "Line-of-Sight Rate Estimation and Linearizing Control of an Imaging Seeker in a Tactical Missile Guided by Proportional Navigation," IEEE Transactions on Control Systems Technology, Vol. 10, No. 4, 2002, pp. 556-567. doi:10.1109/TCST.2002.1014675 (Pubitemid 34798678)
    • (2002) IEEE Transactions on Control Systems Technology , vol.10 , Issue.4 , pp. 556-567
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  • 11
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    • Inst. of Electrical and Electronics Engineers, Piscataway, NJ, doi:10.1109/CHICC.2006.280726
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  • 12
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    • Empirical virtual sliding targetguidance law design: An aerodynamic approach
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.