Guidance Laws for Short-Range Tactical Missiles

Pastrick, Harold L.; Seltzer, S. M.; Warren, Molly

doi:10.2514/3.56060

Cited by 105 publications

(22 citation statements)

References 53 publications

Supporting

Mentioning

Contrasting

Order By: Relevance

“…In the current section, by using the SDRE method, a suboptimal control law is derived for the nonlinear system (7). Using direct parameterization of f(x)=A(x)x and g(x)=B(x), the nonlinear equation (7) can be transformed to the SDC form as follows: (10) Apparently, the choice of the matrix A(x) is not unique and this may lead to a suboptimal controller [22]. This method requires that the pair {A(x), B(x)} is point wise controllable.…”

Section: Optimal Control Design Based On the Sdre Techniquementioning

confidence: 99%

See 1 more Smart Citation

A Novel Nonlinear Robust Guidance Law Design Based On SDRE Technique

Moosapour¹,

Alizadeh²,

Khanmohammadi³

et al. 2012

International Journal of Aeronautical and Space Sciences

View full text Add to dashboard Cite

A nonlinear robust guidance law is designed for missiles against a maneuvering target by incorporating sliding-mode and optimal control theories based on the state dependent Riccati equation (SDRE) to achieve robustness against target accelerations. The guidance law is derived based on three-dimensional nonlinear engagement kinematics and its robustness against disturbances is proved by the second method of Lyapunov. A new switching surface is considered in the sliding-mode control design. The proposed guidance law requires the maximum value of the target maneuver, and therefore opposed to the conventional augmented proportional navigation guidance (APNG) law, complete information about the target maneuver is not necessary, and hence it is simple to implement in practical applications. Considering different types of target maneuvers, several scenario simulations are performed. Simulation results confirm that the proposed guidance law has much better robustness, faster convergence, and smaller final time and control effort in comparison to the sliding-mode guidance (SMG) and APNG laws.

show abstract

Section: Optimal Control Design Based On the Sdre Techniquementioning

confidence: 99%

“…An optimal midcourse fixed-interval guidance law without velocity constraints has been developed for intercepting a target with a constant acceleration vector in [8]. An extensive literature review on guidance laws and OGLs have been performed in [9][10].…”

Section: Introductionmentioning

confidence: 99%

A Novel Nonlinear Robust Guidance Law Design Based On SDRE Technique

Moosapour¹,

Alizadeh²,

Khanmohammadi³

et al. 2012

International Journal of Aeronautical and Space Sciences

View full text Add to dashboard Cite

show abstract

“…As already mentioned, a classical text on missile guidance concepts is (Locke 1955), while more recent work include (Lin 1991), (Shneydor 1998), (Zarchan 2002), (Siouris 2004), and(Yanushevsky 2008). Relevant survey papers include (Pastrick et al 1981), (Cloutier et al 1989), (Lin & Su 2000), and (White & Tsourdos 2001). Also, very interesting personal accounts of the guided missile development during and after World War II can be found in (Haeussermann 1981), (Battin 1982), and(Fossier 1984), while MacKenzie (1990) and Westrum (1999) put the development of guided missile technology into a larger perspective.…”

Section: Guidancementioning

confidence: 99%

Guidance Laws for Autonomous Underwater Vehicles

Breivik¹,

Fossen²

2009

Underwater Vehicles

View full text Add to dashboard Cite

“…and, other guidance methods including the use of differential game theory [3,4]. Missileguidance laws assume that the future trajectory of the target is completely defined either analytically or by a probabilistic model [5][6][7].…”

Section: A Guidance-based Interceptionmentioning

confidence: 99%

Advanced Predictive Guidance Navigation for Mobile Robots: A Novel Strategy for Rendezvous in Dynamic Settings

Kunwar

Benhabib

2008

International Journal on Smart Sensing and Intelligent Systems

View full text Add to dashboard Cite

Abstract-This paper presents a novel on-line trajectory planning method for the autonomous robotic interception of moving targets in the presence of dynamic obstacles, i.e., position and velocity matching (also referred to as rendezvous). The novelty of the proposed time-optimal interception method is that it directly considers the dynamics of the obstacles as well as the target in its interception maneuver: the velocities and accelerations of the obstacles and the target are predicted in real-time for potential collisions. The method is designed to deal with highlymaneuvering obstacles and targets. The interception maneuver is computed using an Advanced Predictive Guidance Law.Extensive simulation and experimental analyses, some of which are reported in this paper, have clearly demonstrated the time efficiency of the proposed rendezvous method.

show abstract

Guidance Laws for Short-Range Tactical Missiles

Cited by 105 publications

References 53 publications

A Novel Nonlinear Robust Guidance Law Design Based On SDRE Technique

A Novel Nonlinear Robust Guidance Law Design Based On SDRE Technique

Guidance Laws for Autonomous Underwater Vehicles

Advanced Predictive Guidance Navigation for Mobile Robots: A Novel Strategy for Rendezvous in Dynamic Settings

Contact Info

Product

Resources

About