Generalized Formulation of Weighted Optimal Guidance Laws with Impact Angle Constraint

被引：67

作者：

Lee, Chang-Hun ^{[1
]}

Tahk, Min-Jea ^{[1
]}

Lee, Jin-Ik ^{[2
]}

机构：

[1] Korea Adv Inst Sci & Technol, Dept Aerosp Engn, Taejon 305701, South Korea

[2] Agcy Def Dev, Taejon 305600, South Korea

来源：

IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | 2013年 / 49卷 / 02期

关键词：

Degrees of freedom (mechanics);

D O I：

10.1109/TAES.2013.6494416

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The generalized formulation of weighted optimal guidance laws with impact angle constraint is investigated here. From the generalized formulation, we explicitly find the feasible set of weighting functions that lead to analytical forms of weighted optimal guidance laws. This result has potential significance because it can provide additional degrees of freedom in designing a guidance law that accomplishes the specified guidance objective.

引用

页码：1317 / 1322

页数：6

共 14 条

[1] New proportional navigation law for ground-to-air systems
Ben-Asger, JZ
Farber, N
Levinson, S
[J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2003, 26 (05) : 822 - 825
[2] Ben-Asher I., 1998, Prog. Astronaut. Aeronaut., V180, P25
[3] Bryson A.E., 2018, Applied optimal control: optimization, estimation and control
[4] OPTIMAL PLANAR INTERCEPTION WITH TERMINAL CONSTRAINTS
IDAN, M
GOLAN, OM
GUELMAN, M
[J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1995, 18 (06) : 1273 - 1279
[5] Optimality of Proportional Navigation Based on Nonlinear Formulation
Jeon, In-Soo
Lee, Jin-Ik
[J]. IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2010, 46 (04) : 2051 - 2055
[6] TERMINAL GUIDANCE FOR IMPACT ATTITUDE ANGLE CONSTRAINED FLIGHT TRAJECTORIES
KIM, M
GRIDER, KV
[J]. IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 1973, AES9 (06) : 852 - 859
[7] Generalized vector explicit guidance
Ohlmeyer, EJ
Phillips, CA
[J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2006, 29 (02) : 261 - 268
[8] Exponential criterion-based guidance law for acceleration constrained missile and maneuvering target
Rusnak, I
[J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1996, 19 (03) : 718 - 721
[9] Time-to-go weighted optimal guidance with impact angle constraints
Ryoo, Chang-Kyung
Cho, Hangju
Tahk, Min-Jea
[J]. IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2006, 14 (03) : 483 - 492
[10] Optimal guidance laws with terminal impact angle constraint
Ryoo, CK
Cho, HJ
Tahk, MJ
[J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2005, 28 (04) : 724 - 732

← 1 2 →