WsfOrbitalManeuver.hpp

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// ****************************************************************************
// CUI
//
// The Advanced Framework for Simulation, Integration, and Modeling (AFSIM)
//
// Copyright 2016 Infoscitex, a DCS Company. All rights reserved.
//
// The use, dissemination or disclosure of data in this file is subject to
// limitation or restriction. See accompanying README and LICENSE for details.
// ****************************************************************************
 
#ifndef WSFORBITALMANEUVER_HPP
#define WSFORBITALMANEUVER_HPP
 
#include "wsf_space_export.h"
 
class UtCalendar;
class UtInput;
#include "UtVec3.hpp"
class WsfLocalTrack;
#include "WsfOrbitalEvent.hpp"
#include "WsfStringId.hpp"
class WsfTrackId;

class WSF_SPACE_EXPORT WsfOrbitalManeuver : public WsfOrbitalEvent
{
public:
   WsfOrbitalManeuver(const WsfOrbitalManeuver& aSrc) = default;
   WsfOrbitalManeuver& operator=(const WsfOrbitalManeuver&) = delete;
   ~WsfOrbitalManeuver() override                           = default;

   WsfOrbitalManeuver* Clone() const override = 0;
 
   bool VerifyCondition() const override;
 
   bool EvaluatePreconditions(const wsf::space::OrbitalMissionContext& aContext) const override;
 
   bool EvaluatePostconditions(const wsf::space::OrbitalMissionContext& aContext) const override;

   virtual void ComputeDeltaV(const UtCalendar&              aCurrentTime,
                              const UtCalendar&              aEvaluationTime,
                              const UtOrbitalPropagatorBase& aPropagator,
                              UtVec3d&                       aDeltaV) const {}; // = 0;

   const char* GetScriptClassName() const override { return "WsfOrbitalManeuver"; }
 
   static WsfStringId GetTypeId();

   double GetDeltaV() const override { return mDeltaV; }
 
   double GetRequiredDeltaV(const UtOrbitalPropagatorBase& aPropagator) const override;
 
protected:
   WsfOrbitalManeuver(const WsfScenario& aScenario);
 
   bool InitializeTimes(const UtCalendar& aEpoch, const wsf::space::OrbitalMissionContext& aContext) override;
 
   bool ExecuteEvent(const UtCalendar& aEpoch, wsf::space::OrbitalMissionContext& aContext) override;
   bool EvaluateCompletion(const UtCalendar& aEpoch, const UtOrbitalPropagatorBase& aPropagator) override;
 
   const UtOrbitalPropagatorBase* GetTargetPropagatorPerception(WsfLocalTrack&                           aLocalTrack,
                                                                const wsf::space::OrbitalMissionContext& aContext) const;
   const UtOrbitalPropagatorBase* GetTargetPropagatorTruth(WsfStringId aTargetName, WsfSimulation* aSimulationPtr) const;
 
   double mDeltaV;
   double mRemainingDeltaV;
};
 
#endif